Tag Archives: Experimental

Official classification tag

Spitfire with DB 605A, “Messerspit”

Nazi flag Nazi Germany (1944)

Experimental Engine Testing Aircraft: 1 Converted Airframe

The enigmatic and misunderstood ‘Messerspit’ test aircraft lies at the center of a number of theories, its original purpose largely forgotten. (google.uk)

Introduction

Few aspects of the Second World War have been so misunderstood, misrepresented, and pushed into near mythology as the Luftwaffe’s test programs. Their discussion in less academic circles is dominated by rampant speculation from those who indulge in sensationalist historical stories. With respect to that, one might be surprised to find the bizarre photographs of a Spitfire Mk. VB with a Daimler Benz engine to be one of the few remaining genuine artifacts from an obscure Luftwaffe test program. With so little information publicly available, naturally, the odd plane’s origins, purpose, and performance have been drowned in a sea of speculation. However, while it is often erroneously claimed that the so-called ‘Messerspit’ was some bizarre attempt to combine the best aspects of the two planes, in reality, the aircraft was converted to settle a technical argument which had been raging in Luftwaffe research and development circles since 1942.

Engine Trouble

The history of fighter engine development is one of ceaseless improvement in power and weight which are largely achieved through improving methods of design, production, and the use of better materials. In the case of the Luftwaffe, it was not long until the chase for power was subsumed by the need to develop engines which could more reliably run on inferior materials. Following the end of the battle of Britain in the autumn of 1940, the Luftwaffe soon found itself short of several key materials necessary in building heat and corrosion resistant alloys, most notably nickel, tin, and, later, chromium and cobalt. Nearly all of these materials were available only in limited quantities across Europe, with tin, used in heavy duty piston bearings, being almost totally unavailable. This was further exacerbated by the transition to synthetic gasoline and lubricants, whose properties differed enough from their petroleum counterparts to cause trouble.

In order to cope with the restricted access to these materials, Sparrmetall economy alloys were introduced to ensure the aviation industry would have access to enough materials, albeit ones which would cause a slate of problems. The Bf 109E had nearly finished its production run before the transition to the new materials began and was soon being phased out by the new F model in late 1940, and there the trouble began. The new production DB 601N engines in these would make use of high octane C3 synthetic fuel. However, the engine was neither designed nor properly tested around this, and had instead been developed around the petroleum based C2. Beyond this, its nickel-poor, and thus corrosion prone exhaust valves, coupled with its more fragile piston and crank bearings, would soon create a web of issues that would take weeks to sort out.

A cut away of the troublesome DB 601N engine. (Flight Magazine)

The C3 fuel reacted chemically with the 109F’s rubber bag tank, and, if stored in the tank long enough, would ruin the anti-knock qualities of this fuel. When run on this degraded fuel, these engines soon suffered absolutely horrible mechanical problems, chief of which were violent vibrations which could thoroughly wreck them. The C3 fuel could also cling to the chamber walls after failing to thoroughly disperse through the fuel injectors, and then escape into the oil system. In most other aircraft, the fuel would simply boil away, but the Daimler Benz engine ran cooler than most, and thus the fuel would eventually dilute the oil until it failed to act effectively as a lubricant, resulting in increased wear or catastrophic engine failure in the worst cases.

Expecting the issue to be one of a mechanical nature, the fuel and bag were not seen as the obvious culprit. Rather, the engine mount, the air intake position, and the cooling system were suspect. This guess would be partially correct in the case of the intake. Eventually, they tracked the fuel degradation to the tank and adjusted the fuel injectors. The unreliable engine was then phased out for the DB 601E, which ran on the more common B4 fuel and was installed in the subsequent Bf 109F-3 and 4 models. Almost all Bf 109’s built after this point were run on this more common, lower performance fuel. Prior to this, the F series were restricted from running at emergency power and were at a considerable handicap in combat for much of 1941 and 42. Regardless of this impediment, many Luftwaffe fighter squadrons often found these their most successful years.

The Bf 109G initially provided no real advantage over its predecessor, and its unreliable engine would prove a particular liability in less than ideal settings, like this G-2 in Finland. (asisbiz)

Problems would resurface again when it came time to re-engine the 109 with the new DB 605A. Developed from the DB 601E, the new engine was to be a marked improvement, with its larger displacement, improved supercharger, and higher compression ratios promising a considerable increase in power. However, new material restrictions would sharply curtail the use of molybdenum, tungsten, and especially cobalt. Supplies of which practically dried up when Germany’s largest source in French North Africa had been lost after Operation Torch. Problems new and old emerged, the most egregious of which were exhaust valve failures, which were due to the low nickel content of the components, resulting in rapid corrosion and cracking. There were also lubrication failures, which were made worse after the switch was made from ball to sleeve bearings. The first Gustavs would enter service in early 1942, though they soon had their performance limited, off and on, to prevent engine failure rates from reaching unmanageable levels. As a result of these limitations, the Gustav was initially slower than the plane it was supposed to replace.

Problems were made even worse when the materials in the engines at Daimler Benz’s testing and development facilities did not match those on the production line, leading to considerable delays in destructive testing. It would eventually receive the improvements to allow it to use its emergency power setting, as exhaust valves were chrome plated and the oil scavenge system was improved, but it was clear that any major future increase in engine performance was only possible after a costly and extended development cycle. The DB 605A would finally be released from all restrictions in August of 1943, almost two years after the first Gustav left the factory.

The Blame Game

The DB 605’s flaws would be magnified in the light of a cascade of engine failures. The most publicized incident involved the loss of ace pilot Hans Marseille, who was lost in action after his engine caught fire and he died trying to escape his aircraft. (asisbiz)

Continued development of the Bf 109 was in a very precarious place, as performance improvements were expected without any major increases in engine power. These goals were largely unachievable for the time being, and thus most of those involved would try placing the fault with some other party when the unrealistic plans fell through. Willy Messerschmitt would place the blame with Daimler Benz, whose engines, he claimed, had cooling requirements that were too high, and thus required the use of larger, drag inducing radiators. In part, he was correct in that Daimler Benz’ engines ran cooler, though in doing so, he seems to have neglected issues with the plane’s radiators, which were supplied by other firms. The Bf 109 was fitted with radiators that operated under considerably lower pressures and temperatures than those used on Allied fighters, and were thus very robust, but less efficient. To his frustration, Messerschmitt was unable to increase the efficacy of the system without more efficient, high pressure radiators, which his suppliers were unable to provide.

In 1942, Messerschmitt began an increasingly adversarial correspondence with Fritz Nalinger of Daimler Benz on the state of his engines, and would request that he permit the engine to run at higher temperatures. In a letter sent in December of that year, he would draw a comparison between the ailing DB 605A and the powerful Merlin 61, then in service with the RAF. He placed particular emphasis on the higher operating temperatures and its use of radiators that were 55% smaller than those in service on the Bf 109. He would leave out that British aircraft designers were working with high pressure radiators which were far more efficient than those on his own aircraft.

At a conference with Göring at Carinhall in March of 1943, Messerschmitt would openly lay blame on Daimler Benz and Nalinger, largely reiterating the points from his correspondence. Nalinger would defend the firm by stating they had put their primary focus in designing the engine in reducing the frontal area and maintaining a high power to weight ratio, but he largely side stepped Messerschmitt’s Merlin 61 comparison by extolling the promise of the still in development DB 628. At the end of the meeting, it had become clear that both men would need to work against one another to defend their own reputations. By then, the Bf 109G had been flying for well over a year under strict engine power restrictions.

The Hybrid

To try and prove Messerschmitt wrong, Daimler Benz planned a simple and clear demonstration. They would install one of the firm’s engines in a Spitfire to show that the DB 605A did not require a large radiator to run. The Spitfire in question was EN830, a Mark Vb which had crash landed in the German occupied Jersey Islands in November of 1942. Its pilot, Lieutenant Bernard Scheidhauer, crash landed his plane after being struck by ground fire during a rhubarb raid over Northern France and a fuel leak prevented him from returning to Britain. After ditching his plane, Lieutenant Scheidhauer attempted to destroy the aircraft when it became clear that he was not on a British held channel island, however, there was insufficient fuel to burn the Spitfire. Scheidhauer was subsequently sent to Stalag Luft III, in Poland. He was among those murdered by the Gestapo after the legendary mass escape.

A standard Spitfire Mk Vb. (wikimedia)

The plane was subsequently taken in hand by the Luftwaffe, repaired, and used for trials at the Rechlin test center. It was later pulled from storage for Nallinger’s tests sometime in late 1943. The plane was re-engined with a DB 605A, though much of the rest of the aircraft was left as it was, save for the radio and armament, which were stripped out. All of the work was done at the Daimler Benz Untertürkheim factory in Stuttgart, after which it was delivered to the Luftwaffe for testing at the nearby airfield at Echterdingen. It was no simple effort to re-engine an aircraft, but it seemed to have been managed well. Testing began in the spring of 1944, with the report on the aircraft being finished May 10th.

The modified aircraft retained much of the same equipment, save for the weapons, which were removed. The avionics were likely all replaced with German alternatives. (Valengo)

The plane flew quite well and proved Nallinger right in that the DB 605A could work using a significantly smaller radiator area. It also made for an interesting comparison with the Bf 109’s radiators, as it was found that the high pressure model fitted to the Spitfire Mk V was 50% smaller but provided only 4% less cooling capacity. The tests also showed that the ‘Messerspit’ was about 25 km/h faster at lower altitudes than the original Spitfire Mk Vb thanks to its fluid coupling supercharger, which proved more efficient at low altitude. Between 4 and 6 km in altitude, the standard Mk V proved faster, before its single stage supercharger again proved less capable than the fluid coupling type on the DB 605A. The hybrid aircraft proved to be between 10 to 20 km/h slower than a Bf 109G-6 at all altitudes save for above 10.5 km, where the ‘Messerspit’ held a slightly higher speed and service ceiling. The experimental aircraft also out climbed the Bf 109 at all altitudes, however, this data is not particularly useful as the plane was unarmed and no ballast to account for its absence was installed.

Overall, the experiment produced mixed results, but proved Messerschmitt right. On one hand, the DB 605 ran effectively throughout the tests using radiators significantly smaller than were found on the Bf 109G. On the other, the type of high pressure radiator used on the Spitfire was not something that could be replicated, owing to numerous material and industrial limitations. In the end, it was Daimler Benz’s requirements that the DB 605 run cooler, and the inability of German radiator manufacturers to produce high temperature, high pressure models, that kept the Bf 109 from achieving greater performance. Following the end of the tests, the aircraft was placed in storage and was likely written off after an 8th Airforce bombing raid on the airfield at Etcherdingen on August 14, 1944.

The Ultimate Fighter?

Unfortunately, due to this unique aircraft’s strange appearance and obscurity, it has been at the center of a number of bizarre theories. Perhaps the most popular of these theories is that the Germans were trying to build a plane that blended the strengths of both the Spitfire and the Bf 109. Some go as far as to claim that the Germans had managed to build something superior to both. This first theory can immediately be written off. By early 1944, neither the Bf 109 nor the Spitfire were considered state of the art, or at the forefront of design in either country. They simply would not be considered an acceptable starting point for any new aircraft design.

However, beyond that, the ‘Messerspit’s’ performance was not particularly impressive for its day. In the official tests, it was compared to both an early Spitfire Mk Vb, which was thoroughly obsolete by the end of 1943, and a Bf 109G-6, which was mediocre by the standards of early 1944. Even then, it compared rather poorly with the G-6, possessing only a higher service ceiling while being considerably slower at almost all but the most extreme altitudes, where it held a slim advantage. To add to this, this low altitude performance gap with the Mk Vb only exists when its Merlin 45 engine is limited to +9 lbs of manifold pressure. When that engine was cleared to run at +16 lbs in November 1942, the Mk V exceeded the DB 605A powered ‘Messerspit’ at altitudes below 5.5 km in linear speed by a margin similar to the Bf 109G-6.

Spitfire Mk IX, Fw 190A-8, Bf 109G-6, P-51B (world war two photos, asisbiz, National Archives)
Aircraft (Manifold pressure) Top Speed at Sea level (km/h) Low blower/Speed (km/h) high blower/Speed (km/h) Maximum Output (hp)
Spitfire LF Mk IX Spring 1944 (18 lbs) 540 617 at 3.2km 655 at 6.7km 1720
Spitfire Mk VB Mid 1942 (9lbs) 460  N/A (single stage, single speed) 605  at 6.1km 1415
‘Messerspit’ Late Spring 1944 (1.42 ata) 488 N/A (variable speed SC) 610  at 6.5km 1454
Bf 109G-6 Mid 1943 (1.42 ata) 510 N/A (variable speed SC) 620 at 6.5km 1454
Bf 109G-6AS Early 1944 (1.42 ata) 506 N/A (variable speed SC) 653 at 8.3km 1415
Fw 190A-8 Early 1944 (1.42 ata)  558 578 at 1.5km 644 at 6.3km 1726
P-51B-15 w/ wing racks Early 1944 (67” Hg)  586  656 at 3.1km 685 at 7.2km 1720

*Values for the Spitfire Mk IX and Mustang indicate use with 100 Octane fuel and not high performance 150 octane, which became fairly common after mid-summer 1944 amongst the strategic fighter forces based in England. Likewise, Bf 109G-6 and Fw 190 performance does not reflect the use of MW50 or higher power clearances, respectively, as they were not in widespread use at the time of the tests. Unrelated, the P-51B-15 made for 627 km/h at 6.5 km with wing racks.

Compared to other contemporary frontline fighters of its day, its performance was far less impressive. The contemporary Spitfire Mk IX, with its Merlin 66 running at 18 lbs manifold pressure, outstripped the hybrid aircraft at all altitudes by a much wider margin than the Bf 109G-6. A further comparison with the Fw 190A-8 and P-51B-15 also demonstrates the continued extreme disparity in linear speed against more modern fighters. While the aircraft did demonstrate a very high climb rate, approximately 21 m/s at sea level (a Spitfire Mk IX made for 23 m/s), this can be explained by the lack of any weapons aboard. The Mk Vb was initially equipped with 2 Hispano 20 mm cannons and four .303 caliber Browning machine guns. The absence of these, and other pieces of equipment, reduced its weight by over 300 kg compared to the Mk Vb used in RAF and Luftwaffe performance trials. This resulting lightening of the aircraft, and the subsequent loss of drag with the removal of the protruding wing cannons, more than explains its high climb rate. The plane’s performance overall was very modest, and frankly did not compare well to any of its contemporaries. In the end, despite being a fusion of the Bf 109 and Spitfire, it compared rather poorly to either one.

Another theory presupposes that the plane was part of an effort to actually produce Spitfires for the Luftwaffe. The foundations for nearly all of these claims rest with an often misunderstood quote from the battle of Britain. When Reichsmarschall Herman Göring asked fighter group commander Adolf Galland if there was anything he needed, Galland responded “I should like an outfit of Spitfires for my squadron”. Galland would later clarify in his memoirs that he meant this rhetorically. In truth, he wanted a plane which could serve better as a bomber escort, something he felt the RAF’s Spitfires were better suited to, with their better visibility and low speed handling, than his own Bf 109’s, which he felt were more capable on offensive patrols. Beyond that, reverse engineering and then manufacturing an aircraft which was designed around the industrial standards and practices of another country was totally unfeasible. It also seems rather implausible that anyone would go to the trouble of building an airplane on the basis of an off hand remark made three years earlier.

Construction

A fore view of the experimental plane. (frankenplane)

The ‘Messerspit’ was built using the airframe of a later production Spitfire Mk Vb. The Mk V differed from earlier models in that it used a heavier engine mount to keep up with increases in output from new engines. It was otherwise much the same as the Mk I’s and II’s which preceded it. These planes were fairly innovative during the interwar period, being all-metal and using a semi-monocoque structure, though these features were soon made commonplace in the earliest days of the Second World War.

The fuselage contained the engine, behind which sat the fuel tank, the firewall, and then the cockpit. The tail boom was of a semi monocoque construction and contained the oxygen bottles, and radio. Aboard the ‘Messerspit’, the engine mount had to be reworked to accommodate a DB 605A, the fuel tank was likely changed to fit the new volume, and the instruments and most of the electronics were swapped for German versions. The radio appears to have been removed entirely. In all likelihood, Lt. Scheidhauer most likely smashed the instrument panel when he knew his plane was in enemy territory. Beyond that, they would have needed to convert the voltage to the German standard, and simply replacing all the equipment would have proven easier than modifying all of the existing components. There were also some instruments, like the DB 605’s RPM governor readout, that would not have had a British analogue.

The wings were elliptical with a large surface area, which granted the aircraft an excellent rate of climb and low wing loading. On the ‘Messerspit’, the inboard pair of 20 mm cannons and the outboard four .303 caliber Browning machine guns were removed and the ports were faired over. Most importantly, the radiator under the starboard wing was connected to the DB 605A engine’s oil and coolant lines. The wings were otherwise unchanged. Generally speaking, the better wheel brakes, greater visibility out the bubble canopy, and its wider wheel base would have likely made this a far more pleasant plane to fly than a Bf 109G.

A DB 605A mounted in a preserved Bf 109G-6 (wikimedia)

The engine was a Daimler Benz DB 605A, an inverted, 35.7 liter, V-12. The reason for it being inverted was to ensure the propeller shaft was as low as possible. This would enable a low mounted, centerline cannon to fire through its center without its recoil seriously jeopardizing the aircraft’s stability. They were able to achieve this using direct fuel injection, which was fairly common practice in German aviation by the start of the war, though rare elsewhere. The engine also possessed a high level of automation, which let the pilot manage the engine and most of its associated systems just through the throttle lever. These were essentially a series of linkages between components that adjusted one another as the pilot increased or decreased engine power. As such, it did not possess a true engine control unit, as was used in the BMW 801. Perhaps most impressively, the engine used a single stage, centrifugal supercharger which used a hydraulic coupling for variable transmission. The fluid coupling supercharger automatically adjusted itself barometrically, and was easily the most impressive feature of the engine, allowing it to smoothly adjust for boost as the plane climbed or descended. This allowed the aircraft to avoid the engine performance gaps between certain altitudes that were otherwise encountered with engine superchargers with multiple stages and fixed speed settings. These gaps were the result of running the supercharger at fixed, unnecessarily high speeds for a given altitude.

The engine used B4 87 octane aviation gasoline, as most of the C3 high performance stock was dedicated to squadrons flying Fw 190s. In comparison to the Merlin 45, which was originally in the Spitfire Mk.Vb, it produced 150 bhp more at sea level thanks to the fluid coupling supercharger, which saw lower pumping losses compared to the Merlin 45. The Merlin 45’s supercharger was geared to medium altitude use, and allowed the engine to outperform the DB 605A between approximately 4 and 6 km.

A DB605A mounted in a Bf 109G, cowling removed. (Norwegian air museum)

In spite of these innovative features, the engine’s output was fairly modest for its day. It produced up to 1475 PS, though this was only possible after several major modifications, such as replacing the exhaust valves for chrome plated sets and modifying the oil scavenge system by adding additional pumps and a centrifuge to improve flow and reduce foaming, respectively. Between 1942 and late 1943, the high power settings on almost all of these engines were disabled in order to keep failure rates manageable. The supercharger too would eventually lag behind its contemporaries, as despite its smoothness, its volume became a bottleneck. This was most apparent in comparison to the two-stage, intercooled models of the Rolls Royce Merlin engine. Some later models would mount an enlarged supercharger, taken from the larger DB 603, though the upgrade was not universal. Nearly all would be equipped with an anti-knock boost system in the form of MW50 in the weeks after the ‘Messerspit’s’ tests, which would boost output up to 1800 PS, though the corrosive mixture of methanol and water decreased the engine’s lifespan. Engines with the larger supercharger were designated DB 605AS, those with the boost system being DB 605M, and those with both were 605ASMs. These upgrades gave late war Bf 109’s a good degree of performance after nearly three years of mediocrity. Neither of these upgrades were present on the ‘Messerspit’.

The engine measured 101.1 × 71.9 × 174 cm, had a bore and stroke of 154 mm (6.1 in.) x 160 mm (6.3 in.), and weighed 745 kg (1,642 lb). The aircraft was equipped with the prop spinner from a Bf 109G, used the same supercharger scoop, and was likewise fitted with a two meter VDM propeller. The engine cowling of this aircraft seems to have been built for requirement.

Spitfire Mk V with DB 605A Specification
Engine  DB 605A
Engine Output 1475PS
Gross Weight 2740kg
Maximum speed at Sea Level 488 km/h
Maximum speed at Critical Altitude 610 km/h
Max climb rate at sea level 21 m/s
Max climb rate at FTH at ~6.5km 11 m/s
Crew Pilot
Wingspan 11.23 m
Wing Area 22.5 m^2

Conclusion

Another view of the experiment (Aviationhumor)

In the end, the ‘Messerspit’ was built to serve a single, fairly mundane purpose. It was never meant to set records, achieve any kind of technical breakthrough, or somehow be an unbeatable synthesis of two planes that had already seen their day in the sun. Above all, it was never meant to see combat nor produce a plane that would. Its only battlefield would be a corporate one.

Illustration

The Spitfire Mk V mit DB 605A, better known as the “Messerspit”.

 

Sources:

Primary:

Bf 109G-2 Flugzeug Handbuch (Stand Juni 1942).Der Reichsminister der Luftfahrt und Oberbefehlshaber der Luftwaffe, Berlin. November 1942.

Bf 109G-4 Flugzeug Handbuch (Stand August 1943). Der Reichsminister der Luftfahrt und Oberbefehlshaber der Luftwaffe, Berlin. September 1943.

Bf 109G-2 Flugzeug Handbuch (Stand August 1943). Der Reichsminister der Luftfahrt und Oberbefehlshaber der Luftwaffe, Berlin. October 1943.

Daimler-Benz DB 605 Inverted V-12 Engine. National Air and Space Museum Collection. Inventory number: A19670086000.

Flugzeug Flugleistungen Me 109G-Baureihen. Messerschmitt AG Augsburg. August 1943.

Flugleistungen Normaljager Fw 190A-8. Focke-Wulf Flugzeugbau G.m.b.H. Abt. Flugmechanik.L. October 1944.

Horizontalgeschwindigkeit über der Flughöhe: Normaljäger Fw 190A-8. Focke-Wulf Flugzeugbau G.m.b.H. November 1943.

Leistungen Me 109G mit DB 605 AS. Messerschmitt AG. Augsburg. 22, January 1944.

P-51B-15-NA 43-24777 (Packard Merlin V-1650-7) Performance Tests on P-38J, P-47D and P-51B Airplanes Tested with 44-1 Fuel. (GRADE 104/150). 15 May, 1944.

Spitfire V Steigleitungen. Daimler Benz. Versuch Nr. 1018105428. Baumuster DB.605A. May 1944.

Spitfire Mk. VB W.3134 (Merlin 45) Brief Performance Trials. Aeroplane and Armament Experimental Establishment Boscombe Down. June 1941.

Spitfire Mk. VC AA.878 (Merlin 45) Climb, speed, and cooling tests at combat rating. Aeroplane and Armament Experimental Establishment Boscombe Down. 25 November, 1942.

Spitfire L.F. IX. RAF Aircraft Data Card, 2nd Issue. 28, October 1943. The performance of Spitfire IX aircraft fitted with high and low altitude versions of the intercooled Merlin engine. Aeroplane and Armament Experimental Establishment Boscombe Down. March 1943.

USAAF 8th Airforce Bombing Raid Records.


Secondary:

Scheidhauer, Bernard W.M. Traces of War.

Douglas, Calum E. Secret Horsepower Race: Second World War Fighter Aircraft Engine Development on the Western Front. TEMPEST, 2020.

C. Douglass, personal communication, November 25, 2022.

Price, Alfred. The Spitfire Story. Silverdale Books. 2nd Edition, 2002.

Radinger, W. & Otto W. Messerschmitt Bf 109F-K Development Testing Production. Schiffer Publishing. 1999.

Spitfire EN 830. Lostaircraft.com

Galland, Adolf. The First and the Last. Bantam. 1979.

 

Credits

  • Article written by Henry H.
  • Edited by Stan L. and Henry H.
  • Ported by Henry H.
  • Illustrations by Godzilla

 

Maeda Ku-6

 Empire of Japan (1943)
Experimental Glider Tank – One Mock-up Model

While tanks can provide excellent offensive firepower, they can’t always be easily transported to where they are needed. In the case of Japan during WW2, this was usually achieved by using ships and rail lines to transport them to where they were needed. Facing difficult terrain and disrupted shipping routes, the concept of a flying tank became a promising concept to the Japanese military hierarchy. By transporting tanks via the air, they could potentially offer benefits to the airborne troops, who were often left without proper heavy support. An exploration of this concept would lead to the creation of the Maeda Ku-6 tank glider.

The Concept of Airborne Operations

The American M22 Locust light airborne tank. (Source: Wikimedia)

The practice of dropping airborne troops behind enemy lines offers many tactical advantages, as they can attack weak points and enemy supply lines. This in turn would force the opposing side to redistribute its own forces away from the front to deal with this problem. On the other hand, airborne forces often lack proper artillery or armor support, making them vulnerable to well-equipped and directed enemies. Some nation armies responded to this by employing glider transportable light field artillery and even recoilless, high caliber guns. Transporting armored vehicles proved a more daring task to implement. Most tanks could not be easily carried inside a transport plane or even parachuted due to their weight and size. The American and British responded by developing lightly armored and armed tanks, such as the M22 Locust or the Light Tank Mk VII Tetrarch. The Soviet Union, on the other hand, designed an auxiliary glider contraption that would be used to transport a heavier tank, the Antonov A-40. This principle would also be tested by the Japanese Army during the war, which led to the creation of the Maeda Ku-6 project.

Antonov’s flying tank was unsuccessfully tested by the Soviets. (Source: Wikimedia)

Airborne Japan

The Japanese began the development of cargo glider designs for military use in 1937. Following the successful use of gliders by the Germans during their conquest of the West in May 1940, the Imperial Japanese Army began developing new gliders in June 1940. In response to this, the Imperial Japanese Navy began its own project soon after. In Japanese terminology, these were designated Kakku (English: to glide).

Both the IJA and IJN had and used parachute infantry units. It is important to note that these were relatively small units that were rarely employed in their intended role. For these reasons, their equipment was more or less the same as that of ordinary infantry formations. They saw the most active service during the fight for the Dutch East Indies in 1942. These were mainly used to capture various vital strategic points, such as airfields or weakly defended positions deep in the enemy’s rear line. Following the end of this campaign, the Japanese did not use paratrooper units in their primary role.

Japanese paratrooper IJN units had two notable deployments: in the successful Battle of Manado from 11th to the the12th January 1942, on Celebes Island, also known as Sulawesi, and in the Battle of Timor from19th February 1942-10th February 1943, where IJN paratroopers suffered heavy casualties. Their IJA counterparts were used more as a commando unit and were only ever airdropped during the invasion of Sumatra in February 1942.

Map of Japanese expansion by 1942. Some of these offensive operations also included the use of parachute units, albeit to a limited extent. (Source: https://www.pinterest.com/pin/389350330265435193/)

In 1943, attempts were made to increase their firepower, though, it is unclear how much impact the experiences from the airborne operations of February 1942 had. It was proposed to use specially designed glider tanks that could be flown to their designated target and thus provide necessary firepower to otherwise weakly armed paratrooper formations. In addition, this vehicle could be airlifted to any other theater of war without a need for them to be transported by ships, which were by this time, seriously endangered by the US Navy.

The Maeda Ku-6

The project was initiated by the Army Head Aviation Office in collaboration with the Fourth Army Research Center. The first drawings of this new design were soon ready and were allocated to the Maeda research center for the construction of a working prototype. In the early stage of development, the new tank was to be transported by a specially designed glider. But as Maeda was unable to create a glider that could transport a light tank, and so another solution was needed. Maeda engineers suggested another approach to this problem. As no glider could be developed to carry a tank, maybe the tank itself could be modified to use a glider.

While Maeda was responsible for the glider development, the design of the tank was given to Mitsubishi Heavy Industries. It is unclear if it was a completely new tank design or if Mitsubishi reused some of the existing vehicles that were in service. According to the Japanese Army and Navy Aircraft Complete Guide, the Type 98 light tank was used for the project. This tank was intended as a replacement for the Type 95 Ha-Go, but this was never achieved as it was built too late and in very small numbers.

The Type 98 light tank on which the Ku-6 was allegedly based. (Source: Wikimedia)

Name of the Project

According to E. M. Dyer, the new light tank was designated as So-Ra (Sora-Sha), which could be translated as the “sky” or “air” tank. The whole project would be designated Kuro-Sha, with the Ku and Ro, meaning the number ‘6’, taken from the Ku-6 glider designation. Lastly, the Sha stands for “tank”. An older source, J. E. Mrazek, mentions that the tank design originated in late 1939. According to Mrazek, the tank was initially designated ‘special Tank project 3’. It received the Sora-Sha designation before being changed to Kuro-Sha (English: Black Vehicle).

Technical Specification

The Ku-6 was designed as a tank transport glider. While not specified, it is likely that the Ku-6 would have been made out of wood. Due to the losses of the original documents, not much is known about its overall design. Over the years, historians based on available information devised two different designs of how this contraption may have looked.

The tank itself, due to its nature of use, had to be as light as possible. This means it would have been lightly armored and armed. The So-Ra’s total weight was slightly above 3 tonnes and would have been operated by two crew members. The driver was positioned in the front of the vehicle. He was also responsible for piloting the whole glider. Behind him, in the turret, was the commander, who was responsible for operating the main armament. This small crew would have greatly affected the tank’s overall performance. Given the limitation in size and weight, adding more crew members was not possible. In normal circumstances, the driver’s vision ports would have been small and protected. In this case, he would need to have a good and unobscured overall view of his surroundings. For this reason, he was to be provided with three large viewports. The armor was to be less than 12 mm thick. While its armament consisted of one 37 mm gun, along with a machine gun, a possible installation of a flame thrower was also considered.

The wooden mock-up of the Japanese airborne tank project. (Source: https://www.armedconflicts.com/Maeda-Ku-6-t41347)

As the tracks would cause massive drag during take-off, specially designed sleds would be attached to them to facilitate an easier take-off. According to the first proposals, the tank itself was designed to act as an improvised glider fuselage and the wings and the tail assembly would be attached to it.  The tank crews would be provided with wired controls installed inside the vehicle in order to pilot it. In front of the tank, a towing cable would be added to connect it to the glider tug.

In the first version, the wings were to be attached to the So-Ra sides with the tail assembly to the rear. (Source: https://www.armedconflicts.com/Maeda-Ku-6-t41347 https://imgur.com/a/xaLcNcO)

The second version is completely different. Above the tank, a larger wing with a twin tail boom was added. These two components would be connected by struts. In both cases, once the tank hit the ground, the wing assemblies could be easily removed, which meant that the tank could immediately go into action with relative ease.

The second version was completely different in appearance. (Source: https://www.armedconflicts.com/Maeda-Ku-6-t41347)

It is unspecified which material would be used during the whole wing assembly. Given its rather late introduction and Japanese limited resources at this point, wood would likely be used.  With the whole wing assembly, the Ku-6 had a length of between 12.8 to 15 m (depending on the source) with a width of 22 m and a height of 3 m. The wing area was around 60 m².

The maximum towing speed at heights of 4 km was 250 km/h. The maximum speed that could be achieved during the gliding flight itself was 174 km/h. The decent speed at 4 km altitude was 2.8 sec/m while at lower heights closer to the ground it was 2.6 sec/m. It is important to note that these are projected figures.

Testing and Project’s Fate

Due to the slow pace of work, the first operational glider prototype was completed in 1945. The tank itself was not ready by this time. As a temporary solution, a wooden mock-up of it with ballast was intended to be used instead. The prototype was taken to the sky by a Mitsubishi Ki-21 medium bomber. Almost from the start, the Ku-6 (according to E. M. Dyer the second variant was used) proved to have poor overall flight characteristics, and the pilot had a poor view. Lastly, as it was specially designed to carry the So-Ra, its transport capacity for other vehicles was very limited. The IJA officials quickly became disinterested in the Ku-6, focusing instead on the Ku-7 general purpose glider which looked more promising. Another aspect that we must take into account was the poor state of the Japanese Army in 1945. By this point, it was so battered and depleted, that undertaking an airborne operation was an impossible task. In the end, the Ku-6 would be terminated and the fate of the single prototype is unknown, but it was either scrapped or lost during Allied bombing raids.

The prototype was taken to the sky using a Mitsubishi Ki-21 aircraft. (Source: Wikimedia)
The Ku-7 was a more orthodox glider design. While they were built in small numbers, they would be mainly used for testing and were not used operationally by the Japanese Army. (Source: https://listverse.com/2015/09/29/10-goofy-warplanes-of-world-war-ii/)

Conclusion

The Ku-6 seems like an interesting concept that could have offered a number of benefits to the Japanese in the early years of the Pacific theater. By 1943, when the project was initiated, the war situation for Japan had rapidly deteriorated, with the Allies pressing on all sides. In reality, the Ku-6 proved to be too flawed in design. It was difficult to control and the pilot had poor visibility. Given that it was a glider, it would make an easy target for Allied fighters which, by its construction time, had almost complete air supremacy.

 

Specification Maeda Ku-6
Wingspan 22 m / 72 ft 1 in
Length 15 m / 42 ft
Height 3 m / 9 ft 8 in
Wing Area 60 m² / 645 ft²
Maximum Takeoff Weight 4.200 kg / 9.260 lbs
Maximum Gliding Speed 174 km/h / 108 mph
Maximum Towing Speed 250 km/h
Crew Two pilot/driver and the commander /gunner
Maeda Ku-6 hypothetical side wing configuration
Proposed version with the top wing construction.

 

Credits

  • Written by Marko P.
  • Edited by Henry H. & Medicman11.
  • Illustrated by Godzilla

Sources

  • D. Nešić (2008), Naoružanje Drugog Svetsko Rata-Japan, Beograd
  • E. M. Dyer (2009) Japanese Secret Projects Experimental Aircraft of the IJA and IJN 1939-1945, Midland
  • J. E. Mrazek (1977) Fighting Gliders of World War II, ST Martin Press
  • S. J. Zaloga (2007) Japanese tanks 1939-45, New Vanguard
  • Tomio Hara’s Japanese Tanks 1978
  • Japanese Army and Navy Aircraft Complete Guide
  • L. Ness (2015) Rikugun Guide To Japanese Ground Forces 1937-1945, Helion and Company

Ikarus 453MW

Yugoslavia flag Federal People’s Republic of Yugoslavia (1952)
Experimental Glider – 1 Prototype Built

The experimental Ikarus 453MW glider. [airwar.ru]
Following the end of the Second World War, the newly created Jugoslovenska Narodna Armija JNA (Yugoslav People’s Army) initiated a series of experimental aircraft design programs. These were intended for testing and gaining valuable experience in new jet propulsion technologies. From this initial work, an unusual new glider project, designated Ikarus 453MW, would emerge. Little is known about the purpose of this glider and its defined role.

The Unusual Glider

After the war, the once-proud Yugoslavian aviation industry was in ruin. Most of its firms had been either looted or destroyed, and many of the pre-war designers and engineers had been killed by the Germans during their retreat. The Allied bombing of Belgrade also inflicted further damage to the Yugoslavian industry’s infrastructure.  However, as the Yugoslav Partisans began liberating the country, some production facilities were slowly restored, as was the case with Ikarus in late 1944. The initial steps of the revitalization effort of the shattered Yugoslavia aviation industry were undertaken in late 1945 by the newly established Yugoslavian Air Force Command. A series of aircraft design teams were set up with the aim of creating a base for the new air force.

By the early 1950’s the overall situation changed to the extent that the Yugoslavian Army officials were ready to test various new technologies and designs. During this time, the Generalna Direkcija Vazduhoplovne Industrije GDVI (Directorate General of the Aviation Industry) led by Dragoljub Bešlin produced a series of experimental aircraft intended to test new design concepts. In 1952, work on an unusual inverted gull “M” shamed wing design began. The design team was also supported by the engineer Levačić. He was an experienced designer who worked with the British Royal Air Force during the war .

In the 1950s a series of experimental aircraft were produced including (from the left to the right side) Ikarus 452-2, 451M jet aircraft, and two prone-operated aircraft the Ikarus 451 and 232  acesflyinghigh.wordpress.com

The precise reasons for its commissioning and its history are not clear, but it appears that the Yugoslav army officials wanted to test a design that could offer a small and fast ground attack aircraft. When the design was ready, Ikarus was asked to construct the first glider prototype. If the glider design proved to have merit, the next step would be to equip this aircraft with a fully functional jet engine. It was designated the Ikarus 453MW, but it is also sometimes referred to as Р-453MW or GDVI-9. To avoid confusion this article will use the Ikarus 453MW designation. The MW  designation was used as the wings highly resemble these letters.

Technical Characteristics 

The Ikarus 453MW was a single-seat, mixed-construction experimental glider. Its fuselage was made of a metal base covered with metal sheets. The wings and tail assembly were made out of wood. The most noticeable characteristic of this glider was the use of unusual inverted gull m-shaped wings. The inverted gull wing design was used during the war by famous aircraft such as the German Ju 87 Stuka Japanese Aichi B7A and the American F4U Corsair. The Ikarus 453MW wings consisted of four parts. The part where the wings folded down was separated by two round-shaped gondolas. The wings were equipped with flaps and ailerons. The rear tail unit consisted of a simple rudder on the vertical stabilizer and did not have horizontal stabilizers.

The retractable landing gear consisted of four wheels. Two smaller wheels were located inside the fairly large wing gondolas. In the lower part of the fuselage, an additional and larger pair of landing wheels was located.

The cockpit was placed to the front of the central fuselage. The canopy was made of plexiglass but besides that, little is mentioned of the cockpit design.

While the experimental glider was unpowered, if successful it was planned to add two unspecified jet engines inside the wing gondolas.

 

The side and top drawing of the Ikarus 453MW. The wing design while unusual was not used on any other Yugoslavian aircraft design. Source: www.vazduhoplovnetradicijesrbije.rs
The Ikarus 453MW had a landing gear consisting of three landing wheels units. Two smaller ones are located in the wing gondolas and one in the central fuselage. Source: www.vazduhoplovnetradicijesrbije.rs

Testing and Cancellation of the Project

The Ikarus 453MW prototype was completed and ready for testing by November 1952. On the 28th of November, the first test flight was made by Metodije Bojković. The test flight was undertaken at the Batajnica Airfield near the capital of Belgrade. Unfortunately for all present, an accident occurred. During take-off, the glider veered off the runway. While the pilot was unharmed the glider was damaged and the test flight had to be temporarily postponed.

After repairs were made, additional aerodynamic wind testing was undertaken to test the overall design shape. As these proved satisfying, another test flight was to take place. The Ikarus 453MW was towed up to 3 km of altitude by an Ikarus 213 and then released. While the flight itself was without problems, another accident occurred during landing. After analysis of available data, it was concluded that the pilot was not to blame as he was not properly instructed on how to fly the Ikarus 453MW which had an unusual wing design. Following the second accident, an order was given by the Yugoslav Army officials to cancel the Ikarus 453MW project.

A Nuclear Carrier

Author  N. Đokić (Projektat Jugoslovenskog Strategijskog Bombardera) gives us an interesting reason for the Ikarus 453MW design. It is a generally lesser-known fact, but during this time, the JNA was highly interested in developing nuclear weapons. The JNA’s involvement in Yugoslavian nuclear research development is to this day still not completely clear. This source mentioned that according to some secret JNA documents, the Ikarus 453MW was intended to be an aircraft that could quickly deliver a nuclear warhead to enemy targets. For this reason, the final aircraft was to be able to carry one 2-ton nuclear warhead at a speed of 850 km/h. The operational range was to be some 2,000 km, and the maximum service ceiling was 11,000 meters. In the meantime, a contingent of F-84G jet aircraft was acquired from the United States. As these were capable of carrying nuclear weapons there was no need to further proceed with the Ikarus 453MW project.

Whether there is any truth to the nuclear weapons plans is difficult to determine. The JNA and the Yugoslavian political hierarchy were publicly known to be quite interested in developing nuclear capability. Of course, this would demand a massive amount of resources, highly trained personnel, and well-developed industrial capacity, all of which Yugoslavia simply lacked in these early years of its existence. Its industrial capacity and infrastructure were almost completely destroyed during the war, and it would likely, if at all possible, take decades of commitment and investment to actually build a nuclear weapon. Hypothetically, even if Yugoslavia was able to develop nuclear weapons in the following decades, all research and experience gained on the Ikarus 453 would be outdated by that time. In conclusion, it could not be ruled out that the JNA had overzealous and ambitious plans to test the concept of using a swift aircraft to deliver this weapon. In reality, Yugoslavia simply lacked any means to actually produce such weapons. Despite this, testing this unusual wing design, albeit in a limited manner, at least provided Yugoslav aircraft engineers with additional experience.

Surviving Model

While unfortunately the Ikarus 453MW glider was not preserved, a small model replica is on display at the Nikola Tesla Serbian Aviation Museum near Belgrade.

The Ikarus 453MW wooden replica is located in the Belgrade Aviation Museum. Source: www.vazduhoplovnetradicijesrbije.rs

Conclusion

The Ikarus 453MW was quite an interesting design mostly due to its unusual wing shape. Its overall history, especially the trials is somewhat obscure. While the prototype was involved in two accidents, this was not the fault of the design but rather poor communication with the pilot, who was not informed of its flight characteristics.

Specification Ikarus 453MW
Wingspan 7.5 m /  24 ft 7 in
Length 5.85 m / 19 ft 2  in
Height 2.01 m /  6 ft 7 in
Maximum Takeoff Weight 1,720 kg / 3,792lbs
Crew One pilot
Armament
  • None

 

Experimental Ikarus 453MW

Credits

  • Written by Marko P.
  • Edited by Henry H. & Ed J.
  • Illustrated by Carpaticus

Sources:

Heinkel He 176

Nazi flag Germany (1937)
Rocket Powered Aircraft – 1 Prototype Built

For many years artists often imagined that the He 176 would have looked something like this. [luft46.com]
Prior to, and during the war, the German aviation industry developed a series of operational and prototype aircraft designs. Among the leading new technologies, rocket-powered aircraft were being developed. The concept was initially tested prior to the war on a smaller scale, including limited theoretical tests and prototyping. But further development would lead to the creation of the first rocket-powered aircraft known as the He 176. While it wasn’t accepted for service, it proved that such a concept was feasible and set the stage for the later Me 163 rocket-powered aircraft.

History of Rocket Engine Development in Germany

Following the end of the Great War, Germany was forbidden to have an Air Force. This also included the development of aircraft designs, though this did not stop the Germans from experimenting with new aviation technology. One such new technology was rocket propulsion. One of the first such flights using rocket propulsion occurred in June of 1928, when aviation enthusiast Fritz Stramer took to the sky his rocket-powered glider. Another pioneer in rocket-powered flight occurred at the end of September 1929. A pilot named Fritz von Opel managed to take to the sky in his rocket-powered glider, named Ente (Duck). Von Opel was assisted by another prominent aircraft designer Alexander Martin Lippisch. While technically speaking these were not real rocket-powered flights, given that these gliders did not take to the sky using purely the rocket engine but were towed to altitude. Nevertheless, these flights showed that flight using rocket engines was possible.

Von Opel experimental take-off using a rocket propulsion. [L. Warsitz The First Jet Pilot]
Over the following years, Lippisch became quite interested in rocket technology and would join the Deutsche Forschungsinstitut DFS, where he worked as an engineer. There, he developed a series of new glider designs, like the DFS 40. This work would eventually lead to the creation of the Me 163 rocket-powered aircraft. The Junkers Aircraft company also was interested in rocket development as they built and tested rocket take-off boosters. One such engine was ground tested in 1936.

Another stepping stone in rocketry research was the work of Wernher von Braun. In 1932 and 1934 von Braun managed to successfully launch two rockets using liquid-fuel rocket engines. In 1935 he managed to come into contact with Dr. Ernst Heinkel 1935. After von Braun presented his work, Dr. Ernst was highly impressed and promised to provide von Braun with any assistance in his work. For this, he appointed a young and energetic aircraft engineer named Walter Wenzelunzel to assist von Braun. In order to properly test the installation of rocket engines in aircraft designs, a special test center was established at Kummersdorf in 1936.

The He 112 prior to the start of testing with the von Broun rocket engine. [luft46.com]
Dr. Ernst supplied this research team with a few He 112 airframes. The first He 112 was used for ground testing. For this reason, its fuselage was retained while its wings and the original engine were removed. The rocket engine, which ran on a combination of liquid oxygen and alcohol, would be placed in the rear of the fuselage, with the engine nozzle being placed just beneath the tail unit. Von Braun’s team installed the oxygen tanks in front of the cockpit, with the alcohol tank behind the pilot seat. The engine (the sources do not specify its precise designation) could provide a thrust of 1,000 kg (2,200 lb) with an endurance of 30 seconds. During the testing the engine exploded, destroying the aircraft in the process.

Despite this setback, the project went on. By this time, German Army Officials were becoming interested in the project. In order to maintain its secrecy, von Braun and his team were instructed to find a remote auxiliary airfield where these tests could continue to be conducted away from prying eyes. The team, wanting to be close to Berlin, chose a small field at Neuhardenberg, which was covered on most sides by dense forest. Temporary housing, cabins, and tents were quickly set up in 1937 and the work could finally go on.

In 1937 von Braun began close cooperation with another enthusiast of rocket engine development, Helmuth Walter. This cooperation was partly initiated by the German Air Ministry (Reichsluftfahrtministerium RLM) who intended to use the rocket engines for other proposals, like assistance during take-offs. Walter was a young scientist who was highly interested in rocket propulsion. He managed to obtain military funding, which greatly helped in his work. In 1936 he used a Heinkel He 72 to test this engine. In 1937, he even managed to get the attention of the RLM. The RLM formed a Special Propulsion System department (Sondertriebwerke) with the aim of experimenting with rocket engines in the aircraft industry. While this department was mainly focused on developing rocket engines for short take-off assistance, Walter wanted more than that. He intended to develop a strong rocket engine that could replace the standard piston engines of the day. Walter managed to develop such an engine, named Walter TP-1, which was fueled by the so-called ‘T-Stoff’ (hydrogen peroxide) and ‘Z-Stoff’ (water solution of either calcium or sodium permanganate).

Von Braun requested another aircraft which Henkel provided, this was the He 112 V8 (during these trials it received a slightly changed designation V8/U). The test pilot Erich Warsitz managed to take it to the sky using the aircraft’s original piston engine. Warsitz was a crucial pilot for the German early rocket and jet engine development, being heavily involved in testing and helping with the overall design of both the He 176 and He 178. At about 450 meters Warsitz activated the rocket engine, and during the 30 seconds of the engine burn phase, a speed of nearly 400 km/h (or 460 km/h (286 mph) depending on the source) was reached. Due to the dangerous leakage of the engine, the flight had to be aborted, but otherwise, the flight has deemed a success. This He 112 V8 would be returned to Heinkel, but two more aircraft (H7/U and A-03) would be donated to the rocket research program.

Test pilot Erich Warsitz whose experience and work proved to be vital for both He 176 and 178 aircraft development. [firstjetpilot.com]
After this flight, all further tests were conducted using the Walter TP-1 rocket engine. In contrast to the von Braun engine which used alcohol and liquid oxygen as fuel, Walter’s own engine used hydrogen-peroxide and calcium permanganate as a catalyst. This engine was deemed safer too, which is somewhat ironic given the corrosive and volatile fuel. To avoid accidentally coming into contact with the Walter engine fuel, the pilot had to wear a highly protective suit. If exposed to the corrosive fuel, it caused disintegration without actually burning.

More tests were conducted at this location until the end of 1937, when the research was to be moved to Peenemunde. Due to some delays, the tests on the He 112 continued on from April 1938.

Heinkel’s First Rocket-Powered Aircraft

Following the series of tests on the He 112, some officials from the RLM began showing great interest in the prospect of using a rocket-powered aircraft interceptor. It was originally hoped that this aircraft would be capable of vertical, or nearly vertical take-off. When sufficient altitude was reached, the aircraft was then to make a swift dive on its target, firing a volley of its full weapon load. After this attack run, it was simply to glide away once it was out of fuel, to its base of operation.

The work on the project was conducted under a veil of secrecy and began in 1936 at the Heinkel Rostock-Marienehe work. The following year the first drawings of the He 176 V1 (derived from “Versuchsmuster 1” meaning “Experimental Model”) were completed by Hans Regner. Interestingly the designers set a huge task in front of them, by actually trying to reach a blistering speed of 1000 km/h (620 mp/h). An astonishing and difficult feat to achieve with such a novelty design. This set a number of challenges that had to be overcome. One of them was a proper wing design able to withstand the pressure of such high speed. For this reason, it had to be designed to be flat, at only 90 millimeters thick, with very sharp leading edges. This in turn caused further problems, as this design would cause the aircraft to stall at low speeds. In addition, the installation of wing fuel tanks would be difficult.

In order to make the whole design smaller and thus save weight, the pilot had to be placed in a rather unpleasant semi-recumbent position, with his legs stretched out in front and the pilot’s seat reclined. This was also done to help the pilot better cope with the extreme G-forces that he would be subjected to during the extremely high forward acceleration. The fuselage had a very small diameter of only 0.8 meters (2ft 7in) and was specially designed according to the height of the test pilot, Warsitz.

The construction of the first prototype was undertaken at the Heinkel’s aircraft works in Marienehe. Once the aircraft was completed, it was to be transported to Peenemunde. The aircraft’s testing was conducted under great secrecy and was transported there via military escort in June 1938. Just prior to the actual testing, Warsitz was informed by RLM officials that given the experimental nature of the design, and Warsitz’s valued status as an experienced test pilot, he was advised not to fly it. Warsitz, who was heavily involved in the He 176 design, protested to Air Minister (Reichsluftfahrtministerium) Ernst Udet, who gave him permission to undertake the first flight. After this was settled, there were some delays with the assembly and engine adjustment.

The initial tests were undertaken on the ground. Due to unsuitable terrain and lack of a proper towing vehicle, ground testing proved ineffective. So it was decided to use the aircraft’s own engine for these tests, which were conducted at the end of 1938. Using the He 178’s own engine on the ground presented a new problem, namely the rudder could not provide steering during take-off. As the aircraft had no propellers to generate airflow, steering the aircraft using the rudder on take-off was ineffective, thus the only way to maintain the aircraft’s heading was by using the left and right brakes on the main wheels. This was quite dangerous for the pilot and the aircraft, as an imbalanced braking force could potentially lead to an accident. The result of the initial testing showed that some changes to the overall structural design were needed. For this, the Heinkel crews spent the winter of 1939 modifying the He 178.

First Flights

During the Spring of 1939, a series of small test flights were conducted with the He 178. Somewhat unexpectedly, the Heinkel team was visited by an RLM delegation led by Udet himself. After observing the He 178 on the short flight they were quite impressed, but surprisingly for the Heinkel team, Udet forbade any more flights on it. Mostly due to fear for the pilot’s life. After some delays, Warsitz visited Udet in Berlin and filed a plea that the project should go on. Udet finally accepted this and gave a green light.

A military delegation led by Udet observed the He 176’s initial short flight attempts. The man in the white suit is the test pilot Warsitz who is speaking with delegation members about the flight, with Dr. Ernst just behind him. [luft46.com]
While the first official flight of the He 176 was to be conducted under the supervision of many RLM officials, feeling that something might go wrong, Erich Warsitz and Heinkel’s team (without the knowledge of Dr. Erns) decided to perform the flight in secrecy. The date for this was set on the 20th of June, 1939. After a rough take-off, the pilot managed to take the He 176 to the sky. Given the small fuel load, the flight lasted around a minute. Overall, the first test flight was deemed a success. The following day, Udet and his delegation visited the site and observed another test flight.

The Fuhrer Inspects the He 176

Hitler during his inspection of the He 176.[L. Warsitz The First Jet Pilot]
A couple of days later Warsitz and Heinkel’s team were informed that any further flights were forbidden. The reason was that Hitler himself became interested in the project and wanted to personally see the aircraft. The He 176 was to be transported to the Rechlin Secret Test Center and shown to many high-ranking members of the Luftwaffe. On the 3rd of July 1939, the aircraft was to be demonstrated to a large delegation including Hitler himself. First, a flight of a He 111 equipped with rocket-assisted take-off was shown to Hitler, which greatly impressed him. Another Heinkel innovative design, the He 178 jet-engine powered aircraft, was also present. While it was not yet capable of taking to the sky it was used for ground testing. Next in the line for inspection was the He 176, after a brief examination of its interior by the delegation, the stage was set for it to take to the sky. The flight initially went well, but the pilot miscalculated and shut down the engine too soon. While still at high speed, he began descending rather rapidly. After several attempts to restart the engine, he finally succeeded, just before hitting the ground. The plane took an almost vertical climb of some 50 meters before the pilot regained control and landed it safely. Hitler and his delegation were under the impression that the pilot performed this maneuver intentionally to demonstrate the aircraft’s potential. For his flight, the pilot was awarded 20,000 Reichsmarks.

The End of the Project

After this exhibit, Heinkel’s team tried to prepare the He 176 for reaching speeds up to 1,000 km/h. Structural analysis of the design, on the other hand, showed that this would not be possible. For this reason, preparation for the construction of a second prototype was underway. It was to be powered by a von Braun rocket engine, which suggested that the aircraft could be launched vertically. This was possible thanks to weight reduction efforts sufficient to enable vertical take-off.

Ultimately the whole project would be canceled. The order was given by Adolf Hilter, who insisted that designs that could not enter production in less than a year, be canceled. Despite Heinkel’s attempt to win over Udet’s support, it went nowhere and the project was officially terminated.

The He 176 V1 was disassembled and transported to the Aviation Museum in Berlin to be exhibited. Sadly it would be later on destroyed in one of many Allied bombing raids. The He 176 V2 was almost complete, but its parts were eventually scrapped. The V3 had also been under construction, but was ultimately abandoned in its early stages.

Technical Characteristics

The He 176 was designed as an all-metal, high-wing rocket-powered experimental reconnaissance aircraft. Its fuselage had a simple circular cross-section design. The wings had an asymmetrical profile and were quite thin. During take-off, there was a significant chance of the wingtips contacting the ground, due to the fuselage’s small diameter and extreme vibrations during take-off. To avoid damaging them, Heinkel engineers added a “U” shaped metal bar under each wingtip as a temporary solution. The wings were also initially to act as fuel tanks, but this feature had to be abandoned on the prototype, and fuel was instead stored behind the cockpit. The tail and rudder design was more or less conventional.

To avoid causing damage to the wings during take-off, Heinkel engineers added a “U” shaped metal bar under each wingtip.

The rocket engine chosen for the He 176 was the Walter RI type. It provided thrust ranging between 45 kg to 500 kg (100 to 1,1100 lb) with an endurance of one minute. Due to the weight issues combined with a relatively weak propulsion unit, the desired speed of 1,000 km/h (620 mph) was never reached. The maximum speed reached by this aircraft differs greatly between sources. For example, D. Nešić mentioned that the maximum speed was only 345 kmh, while authors J. R. Smith and A. L. Kay quoted a figure of 700 kmh. Lastly, the test pilot himself in his own logbook mentioned that he managed to reach a speed of 800 kmh (500 mph).

The landing gear consisted of one front smaller wheel, two larger wheels 700 mm in diameter, and one more to the rear. While the front wheel was fixed the remaining three were completely retractable.

The He 176 during take-off [L. Warsitz The First Jet Pilot]
The cockpit provided the pilot with an excellent forward view and was made of plexiglass. Given the experimental nature of this aircraft, great attention was given to pilot safety. As in case of emergency, bailing out of the fast-moving and cramped aircraft was almost impossible. Heinkel engineers designed the entire cockpit section to be jettisonable. The cockpit assembly was connected to the fuselage by four locks which were equipped with small explosive charges. When the pilot was jettisoned from the fuselage his parachute would open automatically and allow him to land safely. This system was tested by using a wooden cockpit containing a dummy pilot. This trial cockpit was then taken to the sky by a He 111 and at sufficient height, it was released. The parachute opened without an issue and it landed on the ground intact. The results of the dummy pilot showed that this system was safe if the cockpit landed on soft ground.

The small size of the cockpit prevented the use of a standard instrument panel, as it would severely affect the pilot’s forward visibility. Instead, the instruments were placed to the left and the right of the pilot. Interestingly, while Heinkel did not intend to arm the aircraft, RLM officials insisted that two machine gun ports be placed beside the pilot. Due to the cramped cockpit interior, the two machine guns had to be placed where the pilots’ side controls were positioned. As this would cause delays and much-needed redesign work, the Heinkel engineers simply placed machine gun ports (without the actual machine guns equipped) and kept the original control units in place. The RLM officials, when visiting the work, were told that these were just temporary measures.

The Only Photograph

The real He 176 was quite different in design. [luft46.com]
Given the secretive nature of the project, RLM officials effectively gathered all films and photos for themselves. All persons involved in the project were also forbidden from taking any pictures. At the war’s end, the Soviets either destroyed or captured these and their final fate is unknown. Sometime after the war, many artists attempted to produce sketches of how the He 176 may have looked. These greatly differed from the original design, but given the lack of information and general obscurity of the He 176, this is understandable.

Conclusion

The He 176 project arose as a collaboration of several different parties. It was heavily influenced by rocket engine testing and development done by von Braun and Walter. Heinkel Flugzeugwerke provided the necessary resources and production capabilities, while test pilot Erich Warsitz provided valuable feedback which guided necessary changes and improvements to the design.

It was a novel idea to use rockets to power aircraft, which offered numerous advantages, such as reaching high speed and altitude very quickly. Given that this project was more or less a Heinkel private venture in the development of new technologies it likewise did not find a place in German military service. It, however, did set the stage for future designs like the Me 163, which actually saw some combat during the war.

He 176 Specifications

Wingspans 4 m / 13 ft 1 in
Length 5 m / 16 ft 4 in
Height 1.4 m / 4 ft 7 in
Wing Area 8 m² / 53 ft²
Engine Walter RI rocket engine
Empty Weight 1,570 kg / 3,455lbs
Maximum Takeoff Weight 2,000 kg / 4,400 lbs
Maximum Speed 700 km/h / 435 mph
Endurance flight Range 60 seconds
Crew One Pilot
Armament
  • None

Gallery

Illustration by Godzilla

Credits

  • Written by Marko P.
  • Edited by Henry H. & Ed J.
  • Illustration by Godzilla

Sources

  • D. Nešić (2008), Naoružanje Drugog Svetskog Rata Nemačka Beograd
  • M. Griehl (2012) X-Planes German Luftwaffe Prototypes 1930-1945, Frontline Book
  • D. Mondey (2006). The Hamlyn Concise Guide To Axis Aircraft OF World War II, Bounty Books.
  • D. Donald (1998) German Aircraft Of World War II, Blitz Publisher
  • J. R Smith and A. L. Kay (1972) German Aircraft of the Second World War, Putnam
  • Jean-Denis G.G. Lepage (2009), Aircraft Of The Luftwaffe 1935-1945, McFarland & Company Inc
  • L. Warsitz (2008) The First Jet Pilot The Story of German Test Pilot Erich Warsitz Pen and Sword Aviation

Sack AS 6

Nazi flag Germany (1943)
Experimental Circular Wing Aircraft – 1 Prototype Built

The unusual Sack AS-6 circular-wing aircraft [falkeeins.blogspot.com]
In the history of aviation there were many designers who had ambitious ideas and concepts for new designs, but never had the chance to bring their ideas to fruition. On the other hand, there were those who had radical or even completely impractical designs that did manage, at least to some extent, to be built. Germany had a fair share of such individuals, especially during the later stages of the Second World War. These designers may have proposed their projects out of desperation to save their country or in fear of being sent to the front. There were also those that were simply enthusiasts in aircraft development but lacked a better understanding of how aerodynamics actually work. One such person was Arthur Sack (1900-1964), who prior to the war came up with the idea of building a circular-wing aircraft known simply as the Sack AS-6.

History

Prior to the war, Germans were prohibited from developing and building military aircraft. The Germans simply bypassed this prohibition by instead focusing on gliders, but also on civilian aircraft which if needed would be quickly converted for military use and conducted secret experiments. They especially took great care in the development and investment of manned gliders, but also scale model-building competitions and organizations. While this may seem like a waste of time and money, it actually helped gain initial and valuable experience in aircraft development which proved vital for the later Luftwaffe.

One such model competition was the National Contest of Aero Models with combustion engines, held in late June 1939 at Leipzig-Mockau. Here, aviation enthusiast Arthur Sack presented his model of an unusually circular-wing-shaped aircraft named AS-1. It is sadly unclear why Sack pursued the design of such an unusual aircraft design. Due to engine problems, the AS-1 was unable to take off from the ground, so the small model had to be launched by hand instead. The Air Minister (Reichsluftfahrtministerium RLM) Ernst Udet, who was present at the event, seemed to be impressed with this design and advised Sack to continue its development.

Arthur Sack and his AS-1 model. [lvz.de]
Thanks to financial support from the RLM, Sack was able to proceed with the development and even the construction of a few scale models, a process that lasted some three years. In 1943 he submitted a fully operational model SA-5 to the RLM. The presentation went well for Sack and the RLM commission provided the necessary funds for the construction of a fully operational prototype. Interestingly, at some point Sack came into contact with another unusual aircraft designer Dr. Alexander Lippisch. While not completely clear, it appears that Sack received some design tips from Lippisch, to better improved his work.

With the order secured, Sack initiated the construction of a prototype. He named this aircraft the AS-6 V1 (Versuchs – version). As he had no proper workshop to build the aircraft himself, the glider manufacturer Mitteldeutsche Metallwerke was tasked with this instead. The initial work for the assembly of the aircraft began in the autumn of 1943. It took nearly half a year to complete the working prototype. Interestingly, due to the general shortage of materials, the AS-6 was constructed by utilizing a considerable amount of salvaged components from other damaged aircraft. For example, the cockpit canopy and parts of the interior were taken from a Bf 109B. Once the prototype was ready, it was allocated to the Luftwaffe for initial tests in early 1944.

AS-6 side view. [lvz.de]

Technical Characteristics

A good view of the AS-6 internal wooden frame construction.[all-aero.com]
The AS-6 was designed as an experimental prototype to test the idea of using circular-wing design. Sadly, this aircraft is quite obscure and poorly documented so not much is known about its overall design. It was a single-seater aircraft that was mostly built out of wood. It did not have a classical fuselage, instead, the majority of the aircraft consisted of two large circular wings. The internal design is more or less conventional with a wooden construction frame being covered with canvas. Two large elevators were installed on the rear of the wings. The tail assembly is a conventional design as well, consisting of one vertical stabilizer and two horizontal stabilizers.

The AS-6 rearview. The two elevators were too small, poorly designed, and did not provide adequate control during initially limited test flights. [all-aero.com]
The AS-6 was powered by an Argus As 10C-3 engine, which ultimately proved to be inadequate [all-aero.com]
The AS-6 was powered by a 240 hp Argus As 10C-3 engine driving a two-blade wooden propeller. The engine was housed in a metal frame, which was then bolted to the AS-6 fuselage. The engine was salvaged from a Bf 108 aircraft.

The cockpit canopy and its interior, as already mentioned, were taken from a Bf 109B. The cockpit was slightly elevated above the fuselage and provided the pilot with an excellent all-around view. The landing gear was also salvaged from a Bf 109B, but in the case of the AS-6, it was fixed. Initially, a landing skid was used on the rear, which was later replaced with a landing wheel instead.

The canopy and landing gear was taken from a damaged Bf 109 aircraft [ufxufo.org]

Testing the Prototype

Initial evaluation tests of the AS-6 prototype were conducted at the Luftwaffe Brandis Airbase. The flight tests were conducted by Rolf Baltabol Junkers test pilot. While several short take-offs were made, there were no attempts to actually take the aircraft to the sky. The test pilot noted that the aircraft had an overall poor design and was difficult to control. He urged that the control surfaces and rudder be completely redesigned. The engine was also deemed too weak. During the last short take-off, one of the two landing gear assemblies was damaged.

The AS-6, following its unsuccessful start, spent several weeks in repairs and received a number of modifications in an attempt to improve its performance. These included adding an additional 70 kg of weight to the rear, installation of brakes taken from a Ju 88, and repositioning the landing wheels to the rear by about 20 cm. Sack proposed moving the landing wheels further back, but the test pilot Rolf simply refused to fly it if this change was implemented. He argued that placing the landing gear to the rear would imbalance the aircraft potentially leading to tipping forward during a take-off. For this reason, the modification was not implemented. While the engine was underpowered, there were simply no alternatives available at that time.

The AS-6 during testing [falkeeins.blogspot.com]
The next test was scheduled for April 1944. During these tests, Rolf tried to take it to the sky, but failed again to do so. This time it was noted that the wings were simply too short. Further tests were canceled, the AS-6 was to await more modifications, and was to be tested in a wind tunnel; if possible with a completely new engine.

The fate of the AS-6

Following the unsuccessful testing, the AS-6 was stored at the Brandis airfield. In the summer of 1944, this airfield became the main operational base for the experimental Me 163 rocket-powered aircraft. The pilots of the I./JG 400 (charged with testing the Me 163) found the AS-6. One of its pilots, Franz Rossle, expressed a desire to attempt flying the unusual plane. But when the ground crew was preparing the aircraft for take-off, one of its landing gear units simply broke due to rough terrain, effectively preventing the test flight to be conducted. After this, it was once again stored at Brandis. It would remain there until early 1945 when it was lost in an Allied bombing raid.

The AS-7 project

While not clear when (possibly during early 1945), Sack approached Messerschmitt company with a proposal to use his circular-wing design on the Bf 109K-4 aircraft. The aircraft marked as SA-7 would be powered by a DB 605 2,000 hp engine. Fitted with circular wings it was theorized that it would be capable of carrying more armament inside the wings. It is believed (but not clear) that Messerschmitt was interested in this proposal and designated the project Me 600. Due to the war’s end, nothing really came from this project.

Conclusion

While certainly an unusual and interesting design, due to poor quality and salvaged materials used during its construction, the AS-6 performed poorly and never actually achieved flight. We will never know if the AS-6 circular-wing design offered any major advantage over more conventional wing designs. It appears that Arthur Sack did not continue with his idea after the war and passed away in the mid-1960’s. While his work was never implemented in mass production, his unusual design was often mistakenly taken as some advanced and secret German World War II project, which ironically, it never was.

AS-6 Specifications

Wingspan 16 ft 5 in / 5 m
Length 21 ft / 6.4 m
Wing Area 19.62 ft² / 211 m²
Engine One 240 hp Argus As 10C-3 engine
Maximum Take-off Weight 1,984 lbs / 900 kg
Crew 1 pilot
Armament
  • None

Gallery

Illustration by Ed Jackson

Credits

  • Written by Marko P.
  • Edited by Henry H. & Blaze
  • Illustrated by Ed Jackson

Sources

  • B. Rose and T. Butler (2006) Secret Projects Flying Saucer Aircraft, Midland Publishing
  • J. Dennis G.G. Lepage (2009) Aircraft of the Luftwaffe 1935-1945, McFarland and Company
  • Duško N. (2008) Naoružanje Drugog Svetsko Rata-Nemacka. Beograd.
  • http://www.luft46.com/misc/sackas6.html

Messerschmitt Me 163D Komet

Nazi flag Germany (1944)
Rocket-Powered Interceptor Prototype – 1 Built

The Me 163D prototype [luftwaffephotos.com]
The Me 163 showed to have great potential as a fast rocket-powered interceptor, but its design had some shortcomings. These included a limited view from the cockpit, lacking of landing gear, increased fuel storage, etc. The German companies Messerschmitt and later Junkers tried to resolve this by implementing a number of improvements to its design leading to the Me 163D of which only a few prototypes were built given the late start of the program.

History 

The Me 163 small size, while reducing the overall cost of the aircraft, enforced limitation of the fuel that could be stored inside which in turn led to a limited operational powered flight time of fewer than 8 minutes. In combat operations, this proved to be insufficient but no auxiliary tanks could be added to the Me 163 wings not inside of it. Another issue was the lack of proper landing gear. The Me 163 was instead forced to use a two-wheel dolly. Once the aircraft was in the air, the dolly was jettisoned. On occasion, there were accidents regarding this system when for example the dolly refused to be detached from the aircraft or even worse when it bounced off the ground and hit the aircraft from below. On the landing, the Me 163 were to use a simple retractable landing skid, placed beneath the fuselage. After landing the aircraft was immobile and essentially an easy target for enemy crafts.  For this reason, a normal retracting landing gear unit was desirable but once again due to Me 163 small size impossible to install.

To redress the previously mentioned issues engineers at Messerschmitt began working on an improved version named Me 163C. It incorporated a longer fuselage, extended cockpit, having an engine with two combustion chambers, and other modifications. The work on this version was rather slow and by war end not much was done on it besides a few incomplete airframes.

Illustration of a Me 163C aircraft, which was to replace the Me 163B. [walterwerke.co.uk]
One or two Me 163B prototypes had their fuselage extended in order if such modification was possible. [walterwerke.co.uk]
Parallel with the Me 163C development another project was carried out in early 1944 once again by Messerschmitt. This project was initially designated as Me 163D and was to have substantial numbers of improvements mostly regarding the overall shape of the aircraft, engine use, weaponry etc. For testing this new concept of substantially extending the aircraft fuselage if it was feasible at all. One or two (depending on the source) Me 163 (BV13 and BV18) was to be experimentally modified with an extended fuselage. In addition, experimental landing gear was also to be added. The testing of this rebuilt aircraft proved to be feasible and so the work on a fully built prototype began in earnest.

Name

The Me 163D project, due to Messerschmitt being simply overburdened with the Me 262 production, would instead be given to Junkers company. Once in their hands, the project was renamed Ju 248. The Me 163D obviously had an identity crisis as in late 1944 it was once again given back to Messerschmitt. Once back to its original designers, the project once again changed its name, this time to Me 263. As all three designations are basically correct for this aircraft, this article will use the original Me 163D designation for the sake of simplicity and to avoid any possible confusion.

First Prototype

Despite being originally designed by Messerschmitt, it was actually assembled in Junkers factories sometime during August 1944 or in early 1945 (the sources are not clear here). After that it would be returned to Messerschmitt where it was planned to examine and test its overall performance. While it was intended to have an increase in fuel capacity and an improved engine, the first prototype had actually no engine installed at that time. The Me 163D V1 (DV-PA) prototype was also provided with a new retractable tricycle landing gear which was to help with the mobility during the ground drive.

Given that no engine was fitted to the Me 163D, first flight testing was done as a glider, in late 1944. After these were conducted the prototype was in a series of wind-tunnel testings. The results of these two test trials (flight and wind tunnel) showed that the Me 163D was not capable of safely achieving dive speeds that were greater than its normal flight speed. In this regard, it was inferior to the original Me 163 aircraft which could achieve extensive dive speed but still managed to preserve good flight controls. The Messerschmitt engineers at this phase even considered redesigning the rear tail unit, but nothing came of it. The tricycle landing gear units did not offer good mobility on the ground, this was mainly due to it being too narrow. The Germans had plans to test using a parachute that was to be released during landing to help reduce the need for a long airfield. If this was tested or even installed on a Me 163D is unknown.

Technical characteristics

The Me 163D like its predecessor was designed as a high-speed, rocket-powered, swept-wing tailless aircraft. Given its experimental nature and its late development into the war, not much is known about its precise technical characteristics. Its overall construction would probably be similar to the previous versions, with a fuselage being built of metal and wooden wings.

The semi-monocoque construction fuselage was longer and was now 7.88 m ( 25 ft 10 in) compared to the original 5.84 m (9 ft 2 in) length. It had a good overall aerodynamic shape. The wings were swept to the back at a 19° angle, compared to the Me 163B 23.3° angle.

The Me 163D like its predecessor had wings that were swept to the back at a 19° angle. The fuselage had an excellent aerodynamic shape. [forum.warthunder.com]
The pilot cockpit received a new ‘bubble-shaped canopy. This provided the pilot with a much greater field of view. Given that it was intended to operate at great heights, the Me 163 D cockpit was to be pressurized and for this was bolted to the fuselage.

The Me 163D received a much better canopy which offered a much better all-around view. It was also completely pressurized so that the pilot could effectively fly it, on great heights. [forum.warthunder.com]
Interior of the Me 163D pilot cockpit. [forum.warthunder.com]
The Me 163D was to be powered by an improved Walter 109-509C rocket engine. It was provided by two combustion chambers.  While the sources are not clear if this engine was ever installed in the Me 163D, the estimated maximum speed was noted to be 950 km/h (590 mph) or up to 1,000 km/h (620 mph) depending on the source. It should also provide more economical consumption of fuel providing an operational range of some 160-220 km (100-140 mile) once again depending on the source. The operational flight endurance was increased from 7 minutes and 30 seconds to 15 minutes.

To overcome the previous Me 163B version’s lack of proper landing gear, the Me 163D was provided with the retractable tricycle landing gear. It consisted of a forward smaller and two larger wheels in the rear, just below the wing roots. All three of these retracted to the rear into the fuselage.

The fuel load consisted of 1040 liters (229 gallons) of T-Stoff and 492 liters of C-Stoff. The Me 163 was notorious for having only a limited endurance flight ofOnce the fuel was spent the pilots were to simply glide the aircraft back to the base.

The armament consisted of two 30 mm (1.18 in) MK 108 cannons, which were placed in the wing roots. Depending on the source the ammunition storage for each cannon ranged between 40 to 75 rounds.

Production

It is often mentioned in the sources that one complete and one partially complete prototype were built, by the war’s end. According to M. Griehl (Jet Planes of the Third Reich)  on the other hand, mentioned that at least three prototypes were built with less than 20 aircraft being in various states of construction when these were captured by the Allies in 1945.

Service

The limited operational test use of the Me 163D  and the German plans for it is not clear. Once again depending on the sources, there are mostly two versions. It appears that despite some faults in its design the Germans were willing to proceed with its further development. Given the end of the war, it should not be surprising that this was ever achieved. In another version, the work on the Me163D after some testing flight in February 1945 was officially terminated by the Luftwaffe officials. Mostly due to the fact that production of its unique and dangerous fuel is no longer possible.

The fate of these aircraft is not clear, given either information that these were either destroyed or captured by the Soviets. The latter option seems more likely as some sources suggest that the Soviets based on the Me 163D after the war developed their own version of it, the I-270. The project led nowhere and it would be abandoned.

    • Me 163D V1 – Completed prototype
    • Me 163D V2 –  Incomplete second prototype
    • Me 163D V3 –  Possible third prototype being built with additional 18 airframes

Conclusion

Given its experimental nature and its late introduction, it is quite difficult to make the final decision on the general properties of this aircraft. While it introduced some improvements in comparison to the previous version it also had issues regarding its reaching speed during dive flights. Despite offering the Germans a relatively cheap aircraft the whole Me 163 project by 1945 was essentially over given the general impossibility of production of its unique fuel. Nevertheless despite its downsides, the Me 163 whole series was certainly an interesting concept that had some merits that unfortunately for the Germans were never completely implemented.

Me 163D V1 Specifications

Wingspans 31 ft 2 in / 9.5 m
Length 25 ft 10 in / 7.88m
Height ft  in  /  3.17 m
Wing Area 192.6 ft² /  17.91 m²
Engine HWL 509  rocket engine
Empty Weight 4,400 lbs / 2,000 kg
Maximum Takeoff Weight 11,660 lbs / 5.300 kg
Maximum Speed 590 mph / 950 km/h
Operational range 100 mil / 160 km
Engine endurance 15 minutes
Maximum Service Ceiling 52,480 ft /  16,000 m
Crew One pilot
Armament
  • Two 30 mm MK108 cannons

Gallery

Artist Conception of the Me 163C – by Carpaticus

Artist Conception of the Me 263 – by Carpaticus

Credits

  • Written by Marko P.
  • Edited by Henry H. & Ed J.
  • Illustrated by Carpaticus

Source:

  • D. Nešić (2008)  Naoružanje Drugog Svetsko Rata-Nemcaka. Beograd.
  • E. T. Maloney and U. Feist (1968) Messerschmitt Me 163, Fallbrook
  • M. Emmerling and J. Dressel  (1992) Messerschmitt Me 163 “Komet” Vol.II, Schiffer Military History
  • J.R. Smith and A. L. Kay (1990) German AIrcraft of the Second World War, Putham
  • http://www.walterwerke.co.uk/walter/me163d.htm
  • W. Spate and R. P. Bateson (1971) Messerschmitt Me 163 Komet , Profile Publications
  • M. Ziegler (1990) Messerschmitt Me 163 Komet, Schiffer Publishing
  • D. SHarp (2015) Luftwaffe secret jets of the Third Reich, Mortons Media Group
  • M. Griehl (1998) Jet Planes of the Third Reich, Monogram Aviation Publication

Kennedy Giant

UK Union Jack United Kingdom (1917)
Heavy Bomber Prototype – 1 Built / 1 Incomplete

The completed Kennedy Giant (Flickr)

The Kennedy Giant was a very large heavy bomber prototype developed by the United Kingdom, and designed by Chessborough J. H. Mackenzie-Kennedy during World War I. The type was meant to be similar to the Russian Ilya Muromets series of heavy bombers. Development was plagued with issues due to the large size of the aircraft, and after a failed attempt at a first flight, the prototype was left to rot. A smaller redesign was in the works, but the program would be canceled in 1920.

The Man

Chessborough J H Mackenzie-Kennedy in front of the Kennedy Giant in 1917. (The Imperial War Musuem Footage)

In 1904, at the age of 18, Chessborough J. H. Mackenzie-Kennedy would leave his home country of Britain and move to Russia. The allure of developing his own aircraft firm in a place where very few firms were located was his main reason to move to the country. Only a few years after moving, Kennedy was able to design and build his own aircraft in 1908, and a year later would establish his own aircraft company, the Kennedy Aeronautic Firm, in 1909. In 1911, Kennedy would become acquainted with Igor Sikorsky, the premier aircraft designer of the Russian Empire. Kennedy would assist Sikorsky on several occasions with the design of several aircraft, but none of these would be as important as Kennedy’s work on the Sikorsky Russky Vityaz. The Russky Vityaz would be the world’s first 4-engined airplane and was one of the biggest aircraft built at the time. The aircraft would first fly in 1913. Kennedy would continue to help Sikorsky work on other aircraft, among them the successor to the Vityaz, the Ilya Muromets, until 1914.

On July 28th, 1914, Europe would be plunged into the First World War, with Britain entering the war on August 4th. After Britain entered the conflict, Kennedy would return to his home country to help with their war effort. Using the knowledge he gained while in Russia working with Sikorsky, Kennedy was confident Britain could use his expertise in aircraft design. Kennedy wanted to create a large bomber, akin to the Muromets. Upon his return to England, he would establish a design office at 102 Cromwell Road, South Kensington in London.

The Machine

Kennedy would begin talks with the British War Council discerning the creation of a large four engine bomber aircraft, similar to projects he had worked on with Sikorsky. Interestingly enough, Igor Sikorsky would convert the Ilya Muromets civilian aircraft Kennedy was familiar with into Russia’s first 4-engine strategic bomber. Kennedy was able to convince the War Council of his idea, and he was given funding to create his heavy bomber. The aircraft would become known as the Kennedy Giant.

The incomplete Giant being worked on. The wings are outside of the hangar while the tail is still inside. (The Imperial War Musuem Footage)

Construction of the Giant began soon afterwards at an unknown date. The manufacture of the components of the aircraft were undertaken by two companies, Gramophone Company Ltd and Fairey Aviation Co Ltd, both located in Hayes, Middlesex. When all of the components were finished, they were shipped to the Hendon Aerodrome for final construction of the massive aircraft. The sheer size of this aircraft would end up being the source of many problems during its development, and the first one would happen upon the arrival of the disassembled plane. Due to its large size, no hangar at the aerodrome was able to house the Giant, so the actual construction of the aircraft was done completely outdoors, on the airfield. The completed aircraft was impressive, possessing an 80ft (24.4m) fuselage and 142ft (43.3m) long wings. The Giant would heavily resemble the Russky Vityaz and Ilya Muromets that Kennedy had worked on in Russia. Due to the large size of the aircraft, the airplane was stored with its tail inside the hangar, whilst its wings and nose protruded outside. Moving the aircraft required two trucks and 70 men, and in one attempt, the fuselage was damaged from this action. The fuselage3 was redesigned to be 10ft (3m) shorter after this. Originally, Kennedy requested the aircraft to have 4 Sunbeam engines for power, but the engines requested were experiencing difficulties during testing, and wouldn’t be operational until after the war. Aside from testing, the War Council didn’t find the Giant important enough to warrant these new engines, and instead four Canton-Unne Salmson Z9 engines were given to the project instead. These engines would power two pusher and two puller propellers. With the engines finally in place, the completed Kennedy Giant was ready for its first flight.

The Kennedy Giant being constructed outside. (Jane’s All The Worlds Aircraft 1919)

The Giant’s first flight was in the later months of 1917. The aircraft would be set in the position for takeoff on the runway, with veteran test pilot Frank Courtney at the controls of the massive machine. The engines were set to full throttle, and as the aircraft gained speed, it only managed to make a short hop off the ground, being airborne for only a moment. It was found that the engines given to Kennedy were not able to take the Giant airborne. With the craft being so ungainly to move, and no desire to give the aircraft better engines, Kennedy’s giant aircraft was abandoned in the fields of the Hendon Aerodrome to rot, with a second attempt at a flight never materializing. Kennedy himself wasn’t discouraged by the failure of his aircraft and he began working on a smaller version that he hoped would achieve flight. Information on this version is sparse, but it was still in development after the war, and despite starting construction, the program was canceled in 1920. No photos or details on this smaller version are known. By 1920 the Giant project was going nowhere. With the war over, the War Council decided such a large aircraft was no longer a worthwhile investment.

A side view of the completed Kennedy Giant. (Jane’s All The Worlds Aircraft 1919)

In 1923, Kennedy would sue the War Council, now the Air Ministry, over a patent he had filed regarding the aircraft. During the war while he was working on the Giant, Kennedy would design a unique system for the tail gunner of the aircraft. The Air Ministry allegedly gave the design plans regarding the Giant to Handley Page in 1917, with the company applying for a patent on the tail gunner position on March 15th, 1918. Kennedy would file for the same patent for his Giant only a day later on the 16th. His case would be dismissed. The last time the Kennedy Giant would be mentioned regarding this case was in an aircraft magazine in 1923, which refers to the Giant still parked at the airfield at Hendon, most likely in poor condition from neglect. An some later date, the Giant was scrapped.

Design

Size comparison shot of the Giant next to a Bristol F.2 fighter. (Jane’s All The Worlds Aircraft 1919)

The Kennedy Giant was a large four engine heavy bomber built using experience gained from the development of the Russian Russky Vityaz and Ilya Muromets. The fuselage of the Giant was of wood construction and was entirely rectangular. All along the sides of the fuselage were celluloid covered windows. The cockpit had several large rectangular windows with good visibility for the pilot. Controls consisted of two large wheels connected to yokes that directed its control surfaces. Located in the upward slope of the nose, there was a window that assisted with bomb aiming. The wings of the aircraft were two bay, meaning a forward and aft row of struts between the upper and lower wings which were covered in fabric, with a wingspan of 142 feet (42.3m). The wings all had the same chord, but the upper wings were longer than the lower. Only the upper wings had ailerons. At the rear of the aircraft were the tail and elevators. Both of these were covered in fabric. The tailfin itself was rather small for the size of the aircraft and most likely would have negatively affected performance had the aircraft achieved sustained flight. The aircraft was powered by four 200 hp ( 149.1 kW ) Canton-Unne Salmson Z9 nine-cylinder water-cooled radial engines powering four wooden propellers. Two of these engines were to be used in a pusher configuration, while the other two were positioned in a tractor configuration.

Despite never being armed, plans for armament of the Giant exist. The aircraft would be armed defensively with 4 machine guns of unknown type. One of these would be located in the nose, one would be located behind the wings on top of the fuselage, and the last two would be in the tail. The tail gunner would have a unique seat option for the gunner, where it could act as either a seat or a kneepad depending on how the gun was being fired. This seat design would be the cause of the lawsuit in 1923. An unknown number and type of bomb would have been used. The bombs would have been held nose down by two arms. A selector gear would control which bombs were dropped while indicating how many were left.

Conclusion

The Kennedy Giant was an earnest attempt to create a heavy bomber using experience gained by Kennedy in Russia, but due to inadequate engines would never be truly realized to its fullest potential. What is interesting to note is the specifications listed for the Giant would actually make it larger than the Zeppelin Staaken R.VI, which is considered the largest production airplane of the World War I. Had it even flown, the Giant would likely have experienced maneuverability issues as its vertical stabilizer height was rather inadequate for the size of the aircraft. After the failure of the Giant, Kennedy would file for bankruptcy, as the program had personally cost him quite a lot of money. He would eventually move to America in the 1930s.

Variants

  • Kennedy Giant – Large, four engine heavy bomber prototype. One built but did not achieve sustained flight.
  • Postwar Kennedy Giant – Very little is known of this variant aside from it being a smaller version of the Kennedy Giant. It was under construction when the program ended.

Operators

  • United Kingdom – The Kennedy Giant was built for the British War Council as a prototype heavy bomber.

Kennedy Giant Specifications

Wingspan 142 ft / 43.3 m
Length 80 ft / 24.4 m
Height 23 ft 6 in / 7.2 m
Engine 4x 200 hp ( 149.1 kW ) Canton-Unne Salmson Z9 nine-cylinder water-cooled radial engines
Propeller 4x 2-blade wooden propellers
Empty Weight 19,000 Ib / 8618.3 kg
Crew 3
Armament

(planned)

  • 4x Machine Guns
  • Bomb Payload of Unknown Size

Gallery

The first version of the completed Kennedy Giant – by Ed Jackson
Closeup view of the cockpit of the Kennedy Giant. (The Imperial War Musuem Footage)
View of the tail of the Giant. (The Imperial War Musuem Footage)
The mid-section of the Giant. (The Imperial War Musuem Footage)
Kennedy demonstrating the controls of the Giant while in the cockpit. (The Imperial War Musuem Footage)
Kennedy walking down the interior of the Giant. (The Imperial War Musuem Footage)

Credits

  • Written by Medicman11
  • Edited by by Ed Jackson & Henry H.
  • Illustrations by Ed Jackson

Sources

  • Grey, C. G. Jane’s all the world’s aircraft, 1919 : a reprint of the 1919 edition of All the world’s aircraft. Newton Abbot: David & Charles, 1969. Print.
  • Mason, Francis K. The British bomber since 1914. London: Putnam, 1994. Print.
  • https://www.wikitree.com/wiki/Mackenzie-Kennedy-7

Belyayev DB-LK

USSR flag USSR (1938-1940)
Experimental Long-Range Bomber – 1 Prototype Built

The Belyayev DB-LK [airwar.ru]
In the late thirties and early forties, the Soviet aviation industry had developed and tested a variety of aircraft design concepts, some quite peculiar. While generally unknown around the world, a number of these strange aircraft would represent a serious departure from anything resembling their contemporaries. Such is the case with Victor Nikolayevich Belyayev’s DB-LK experimental long-range bomber.

History

Victor Nikolayevich Belyayev, March 1896 – July 1953, began working for the Department of the Marine Experimental Aircraft Construction, OMOS, in 1925, where he gained his first experience in aircraft design. In the following years, he worked for the Central Aerohydrodynamic Institute, TsAGl, and Tupolev. During this time, he became an advocate for tailless aircraft designs. He also argued that the so-called “batwing”  or “butterfly”, offered better performance, due to their reduced drag and better stability, than regular wing designs.

The “batwing” design possessed a slightly forward-swept wing with back curved tips. Belyayev managed to construct a glider, designated BP-2, which was equipped with this kind of wing design in 1933, on which he tested this concept. During its test flight, it was successfully towed in the air from Crimea to Moscow, where it proved to have good stability and control during flight.

The BP-2 glider in flight. [airwar.ru]
The next year, Belyayev participated in the competition for a new Soviet military transport plane design. His design was unusual, as it consisted of a large wing and two nacelles,  powered by Tumanskii M-87B 950 hp (708 kW) engines. His design was not approved nor did he build a working prototype. However, four years later, he would reuse this project and adapt it for the role of a long-range bomber. In 1938, he designed the DB-LK long-range flying wing bomber, which the TsAGl approved and ordered the construction of a fully operational prototype. The prototype was built the following year by factory No.156 and by November 1939 it was ready for testing.

Technical Characteristics

The DB-LK had an unusual overall design with no classical fuselage. Instead, the crew, armament, and other equipment were located in the two extended engine nacelles that ended in glazed tail cones (gondolas), somewhat similar to the later German Fw 189. The two extended engine nacelles were, technically speaking, the plane’s fuselage. The semi-monocoque fuselages were constructed by using a combination of metal frames and longerons covered with a duralumin sheet. The DB-LK was designed in this unusual configuration in the hope of reducing the overall drag and weight and thus increasing its speed and range.

The DB-LK’s wings had a unique design, where beside the “batwings” there was an additional center wing section between the two fuselages. Also, the wings were slightly swept to the front with back curved tips. The wings consisted of an airframe covered with light metal stressed-skin. The outer wings had a Gottingen 387 profile, while the center section had a CAHI (TsAGI) MV-6bis profile. The wing edges were curved at an angle of -5° 42′.

A side view of the DB-LK. The strange wing design can be seen. [elpoderdelasgalaxias.wordpress.com]
The rear tail was located on the middle section wing between the two fuselages. The tail consists of one fin and a large 20 ft2 (1.9 m2) rudder. Above the rudder, a smaller tailplane with two, one on each side, large elevators was placed.

A rear view where the large tail and the left glazed rear cone can be seen. [airwar.ru]
One Tumansky M-87B 950 hp (708 kW) 14-cylinder radial engine was installed at the front of both nacelles. For these engines, three-bladed propellers with variable pitch were used. It was planned to upgrade these two with much stronger 1,100 hp (820 kW) M-88 engines, or even the 1.700 hp M-71, but this was never implemented. The fuel was stored in the wing and fuselage tanks, with a total fuel load of 3.444 l.

The landing gear retracted rearwards, with one wheel (900 x 300 mm) in each fuselage. During later testing, the landing gear design was changed with a forward retractable one. This whole landing gear system was operated hydraulically. There was a small fixed rear wheel (450 x 150 mm) located at the bottom of the tail unit.

The DB-LK was to be operated by a crew of four: the pilot, navigator, and the two rear gunners. The pilot position was in the left cockpit and the navigator in the right. The gunners were positioned in both rear glazed cones. One of the two gunners was also the radio operator. The crews entered their positions through roof hatch doors. The two glazed cones could be mechanically rotated 360° by using a small electric engine located at the fuselage top, but the sources do not specify why this was done.

Inside the pilot cockpit [авиару.рф]
The interior of one of the two fuselages. In the picture on the right, the rear machine gun mount can be seen. On the left, the radio and the mechanism that rotated the whole glazed cone can be seen. [авиару.рф]
Both rear glazed tail cones had a recess where a twin  7.62 mm (.30 caliber) ShKAS machine gun mount was installed. These machine guns had a -10 to +10 field of fire in all directions.  Besides these four machine guns, there were two additional ones forward mounted in the leading edge of the center section. These two machine guns were operated by the pilot. In total, around 4,500 rounds of ammunition were provided for these machine guns. The bomb bays were located behind the landing gear doors in each of the two nacelles.

Depending on the sources, the load capacity of the bomb carried is different. The authors Yefim G. and Dimitri K. note that the bomb load was 1000 kg (2,200 lb) with another 1000 kg that could be carried on external racks. According to Bill G., the capacity of each bomb bay (in each fuselage) was one 1000 kg (2.200 lb), two 500 kg (1.100 lb), or smaller bombs with a total of 1000 kg (2.200 lb) weight.

 

Both front and rear views of the DB-LK’s unusual design. [авиару.рф]

Flight Tests

While being completed in November 1939, the first extensive flight test would only begin the following year. This was due to the unwillingness of the test pilot to fly this plane. He did not believe that it was safe to fly due to its unorthodox design. During this time, the plane received the nickname “Kурица” (chicken).

In order to move the entire project testing through this roadblock, the Soviet Direction of the Air Force Scientific test institute, GK Nil WS, appointed M. Nyuikhtikov as the main test pilot, supported by aircraft engineer and test pilot T. T. Samarin and N. I. Shaurov. Under the new leadership, the tests were carried out in the spring of 1940. During the new leadership, the DB-LK was extensively tested in over 100 flights.

During these flights, the pilots managed to reach speeds of 245 mph (395 km/h) at sea level and 300 mph (490 km/h) at an altitude of 16,400 ft (5,000 m). The DB-LK needed a 2,030 ft (620 m) long airfield for landing and taking off. However, the  DB-LK was never truly trialed with a fully loaded payload. The numbers presented above would have likely been different with a full payload of equipment.

The test pilot Nyuikhtikov, after flying on the DB-LK, pointed out some issues with the plane’s design. The main problems were the inadequate overall flight-control system, poor visibility for the pilot and the navigator, especially on the ground. He also noted the poor construction of the landing gear. These reports were examined by the Nil WS Commission led by A. I. Filin. They agreed that the control system should be improved, but Filin had a positive opinion on the landing gear construction. Ironically, during a test flight, where Filin was the pilot, there was a landing gear malfunction during the landing when one of the front wheels broke free, after a possible collision with a treetop. The aircraft was only lightly damaged and the testing continued, but this led to a change in the landing gear design.

There were also other problems mentioned during the tests, like uncomfortable cockpits, low-level of fire protection, structural problems, a limited firing arc of the rear-mounted defense machineguns, and the tendency for the crew compartments to be filled with exhaust fumes from the engines. To solve these issues, there were plans for the DB-LK improvements, with stronger engines, wings, and various other modifications, to be completed by late 1940 but they were probably never implemented.

Rearview of the accident. [авиару.рф]

Conclusion

Despite plans for more testing and improvements, unfortunately for the DB-LK design team, they never got a chance to do so. In late 1940, the Nil WS Commission gave orders for the cancellation of the DB-LK program. The main reason for this was the decision for the production of the Il-4 as the main Soviet long-range bomber.

 

Belyayev DB-LK specifications
Wingspan 70 ft 10 in / 21.6 m
Length 32 ft  1 in /  9.8 m
Wing Area 612 ft² / 65.9 m²
Engine 2x Tumanskii M-87B 950 hp (708 kW) 14 cylinder radial engines
Empty Weight 13,230 lbs / 6,000 kg
Maximum Takeoff Weight 23,530 lbs / 10,670 kg
Fuel Capacity 3.444 l
Maximum Speed 300 mph / 490 km/h
Cruising Speed 245 mph / 395  km/h
Range 790 mi /  1.270 km
Maximum Service Ceiling 27,890 ft / 8,500 m
Climb speed Climb to 3,000 m in  8 minutes
Crew Pilot, navigator, gunner and radio operator/gunner
Armament
  • Six 7.62 mm ShKAS machine gun
  • Two 1,000 kg bombs or Four 500 kg bombs

Gallery

Illustration by Godzilla

Credits

  • Article written by Marko P.
  • Edited by Stan L. & Henry H.
  • Illustration by Godzilla

Sources

  • Y. Gordon, D, Khazanov (1999), Soviet Combat Aircraft Of The Second World War, Midland Publishing
  • Yefim G. and Bill G (2000), Soviet X-Planes, Midland Publishing
  • Peter G. D. (2015), Soviet Aircraft Industry, Fonthill Media
  • D. Nešić (2008), Naoružanje Drugog Svetskog Rata SSSR, Beograd.
  • Aviamuseum

 

 

 

Messerschmitt Me 163A Komet

Nazi flag Nazi Germany (1943)
Rocket Powered Fighter – 10 Built

The first operational Me 163 prototype. [luftwaffephotos.com]
During the Second World War, the Luftwaffe experimented with a number of unorthodox designs. This included a handful of rocket-powered aircraft, like the Me 163. This particular aircraft was created thanks to the somewhat unexpected combination of two different projects. One was the airframe designed by Alexander Martin Lippisch, and the second was the rocket engine developed by Helmuth Walter. Following the testing of the first prototypes, a small series of some 10 aircraft were built that were mainly used for testing and training.

Alexander Martin Lippisch and Helmuth Walter

The history of Me 163 was closely related to the work and design of aircraft engineer Alexander Martin Lippisch and rocket development pioneer Helmuth Walter. Lippisch was somewhat unorthodox in his aircraft design work, to say the least. He was quite interested in the development of gliders and later aircraft that were either completely lacking a tail unit or of an all-wing configuration.

In 1921, Lippisch, together with a colleague, participated in the formation of the so-called Weltensegler GmbH (World Glider Ltd.) company. At that time, the Germans were prohibited from developing and building military aircraft. The Germans worked around this prohibition by instead focusing on gliders and civilian aircraft which if needed would be quickly converted for military use, and conducted secret experiments. While glider development may seem like a waste of effort, it actually provided the Germans with an excellent foundation on which they managed to develop the Luftwaffe during the 1930s, becoming a formidable force at the start of the war. In 1925, Lippisch joined Rhön Rossitten Gesellschaft RRG, where he soon began working on his first glider. It was named Storch I, and incorporated his unusual all-wing design.

Over the years, Lippisch also became interested in rocket technology. With assistance from Fritz von Opel, Lippisch managed to build a rocket-assisted glider. This contraption was flight tested in June 1928. This was actually the first-ever rocket-assisted flight in the world. While initially successful, the glider crash-landed, and caught fire. The plane would be lost in the accident.

This accident did not prevent Lippisch from experimenting with rocket-powered all-wing gliders. He focused his work on a powered version of his Storch V glider. For this project, he used an 8 hp DKW engine. His work was successful and he managed to find investors who were willing to provide funds for the project. This led to the development of the Delta I all-wing aircraft during the late 1920s, and it was followed by Delta II, III, and IV.

Lippisch Delta I prototype. [aviastar.org]
Following this, Lippisch joined the Deutsche Forschungsinstitut DFS, where he worked as an engineer. There, he developed a series of new glider designs, like the DFS 40. In 1938, the work of Helmuth Walter came to his attention. Walter was a young scientist who was highly interested in rocket propulsion. He managed to gain military funding, which greatly helped in his work. In 1937, he even managed to gain attention from the Reichsluftfahrtministerium RLM (German Air Ministry). The RLM formed a Sondertriebwerke (Special Propulsion System Department) with the aim of experimenting with rocket engines in the aircraft industry. While this department was mainly focused on developing rocket engines for short take-off assistance, Walter desired a more prominent role in rocket propulsion. He intended to develop a rocket engine that could replace standard piston engines. Walter managed to develop such an engine, named Walter TP-1, which was fueled by the so-called ‘T-Stoff’ (hydrogen peroxide) and ‘Z-Stoff’ (water solution of either calcium or sodium permanganate). His engine design would be tested in 1939 on the He 176. However, the final results were disappointing and the engine did not go into production.

The DFS 194 predecessor

Lippisch and his design team began working on a new project incorporating the Walter rocket engine. Initially, the project was designated simply as Entwurf X (Design X), before being changed to 8-194 and finally DFS 194. Work on the prototype came to a temporary halt as the DFS lacked proper production capabilities to finish the aircraft. To keep the project going, the RLM instructed Messerschmitt to provide the necessary manpower and production support.

Given the small chance of progression in the DFS and in order to increase the speed of the project, Lippisch and his team moved to Messerschmitt’s base at Augsburg at the start of 1939. He also tried to negotiate with Heinkel for the production and development of the DFS 194 project, but nothing came of this. At Augsburg, Lippisch and his team worked in Messerschmitt’s newly formed Department L (which stands for Lippisch).

The DFS 194 prototype served as the base for the future Me 163. [nevingtonwarmuseum.com]
The first calculations were promising, as the plane would be able to reach a speed of 550 km/h (342 mph). Once completed the DFS 194, was transported to the secret German rocket test center at Peenemunde-West Airfield during the summer of 1939. During ground tests, it was noted that the engine installation was poorly designed and too dangerous to be actually flight tested. Instead, it was decided to use the design as a glider. Surprisingly, despite this huge setback, production orders for three prototypes were given. Initially, these were designated simply as Lippisch V1, V2, and V3, but would be renamed to Me 163A V1 to V3. This was mainly done to mask the true purpose of this aircraft, as this was the name given to an older, rejected Bf 163 Messerschmitt reconnaissance aircraft project.

The Me 163A Prototype Series

The RLM was not satisfied with the general design of the engine compartment initially tested on the DFS 194. They requested that for further Me 163 development, it would need to be substantially changed. In addition, the engine was to be replaced with the Walter R II-203 engine. This engine was to have a manually regulated thrust ranging from 150-750 kg of thrust (330-1,650 lbs). The engine compartment was also to be completely redesigned in order to have easy access to the main components for maintenance.

Following the start of the Second World War in September 1939, the work on the Me 163 slowed down but still went on. The first unpowered flight by the Me 163 V1 prototype, in some sources marked as V4, (KE + SW) was carried out during early 1941. This prototype was towed by a Bf 110 heavy fighter. Once at a sufficient altitude, the V1 was released. During the test flight, the pilot, Heini Dittmar, managed to reach a speed of some 850 km/h (528 mph) during a dive. While this was a great starting point for the project, Hitler, following military victories in Poland and in the West, ordered that funds for such projects be reduced. In the case of the Me 163, this meant that only two more additional prototypes were to be built.

Side view of the Me 163 V1 (V4).[luftwaffephotos.com]
In May 1941, a wooden mock-up of a Me 163 was completed, which was then transported to the Walter Werke. Once there, it was to be equipped with the R II-203 engine. Once the first prototype was fully completed and equipped with this engine, the first tests were carried out at Peenemunde-West in August 1941. The test pilot was once again Heini Dittmar. After a series of test flights that lasted from August to September 1941, the Me 163 prototype showed promising results. The pilot managed to reach top speeds of 800 km/h (500 mph). At this time, the second V2 prototype was also equipped with a rocket engine and used in various test flights. Ernst Udet, Director-General of the Luftwaffe, was highly impressed with its performance. He even gave orders that an additional 8 prototypes were to be built, bringing the total to 13 at this time.

Once the prototype was equipped with the R II-203 engine, the first tests were carried out in August 1941. These proved to be highly successful, which led to an increase in interest for the Me 163 project. [Spate & Bateson]
At the start of October, Heini Dittmar said that, in order to fully test the Me 163’s flying performance, the fuel load had to be increased. On his personal insistence, the V3 (CD + IM) prototype, was fully fueled. This is according to W. Spate and R. P. Bateson (Messerschmitt Me 163 Komet). Other sources like M. Griehl (X-Planes German Luftwaffe Prototypes 1930-1945) this aircraft was described as being the V8 prototype instead. On the 2nd of October 1941, he took to the sky, initially towed by a Bf 110. At an altitude of 3,960 meters (13,000 ft), Dittmar activated the engine. After reaching a speed of 965 km/h (600 mph), he lost control of the aircraft as the result of compressibility effects. The prototype began a rapid descent toward the ground. He then switched off the engine, which enabled him to regain control, after which he landed safely on the ground. Later analysis of the flight indicated that Dittmar managed to reach a speed of 1002 km/h (623 mph). As the whole project was undertaken under great secrecy, this success was not published at the time.

The Me 163 in the middle was the aircraft that Heini Dittmar flew when he reached a speed of 1002 km/h (623 mph). [Spate & Bateson]
Following these events, the Me 163 project got a temporary boost in prominence, with Herman Goring himself placing great interest in it. Ernst Udet additionally placed an order for 70 new Me 163 airframes together with engines for the B version in October 1941. A month later, things changed dramatically for Me 163 after Udet committed suicide. His replacement, Erhard Milch, was less interested in unconventional aircraft designs, like the Me 163. Work on the project nevertheless continued.

A breakup with Messerschmitt

While the Me 163 project was underway, relations soured between Willy Messerschmitt and Lippisch. Messerschmitt personally disliked the Me 163, partly due to its unique overall design, but also given that he was not involved in its development. By 1943, Lippisch left Augsburg and moved to Vienna. While not physically present in the design bureau, he tried to maintain contact with the Me 163 development team at a distance.

In the meantime, Messerschmitt was unwilling to be involved in the Me 163 project, under the excuse that his company was already overburdened with the production of other aircraft. For this reason, the production of further Me 163 aircraft was instead given to Klemm Leichtflugzeugbau, a relatively small aircraft company owned by Hans Klemm.

Production of the A-0 series

While the V1 prototype was mainly used for initial testing, the V2 would serve as a base for the A-0 series. An initial order for ten A-0 aircraft was previously given to Messerschmitt, but only seven were completed. The remaining three aircraft were actually completed by the Klemm factory. These were all completed from 1941 to 1942. The number of prototypes built is not clear in the sources. The numbers range from 1 to 8 prototype aircraft. According to S. Ransom and H.H. Cammann (Jagdgeschwader 400), while three prototypes were meant to be built initially, not all met the requested specifications, except one, which received the V4 designation. Author M. Griehl (Jet Planes of the Third Reich) on the other hand noted that the V4 was the first prototype. He explained that the previous three prototypes were actually related to the initial Bf 163 reconnaissance project that was rejected.

In-Service

Of the 10 built Me 163 A-0 planes, not all were equipped with fully operational engines. A number of them were instead operated as unpowered gliders. This version was not intended for combat operations and was mainly used for crew training and further experimentation.

At the end of November 1943, the V6 aircraft was lost in an accident with the loss of the pilot. In another accident at the end of 1943, another pilot died when the engine stopped working during a takeoff. While the pilot tried to turn back for a landing, having limited control, the aircraft hit a ground station radio antenna before hitting the ground and exploding. It was discovered in an investigation that the undercarriage dolly bounced off the ground much higher than usual, and struck the aircraft, damaging the rocket engine. Some prominent pilots, like Hanna Reitsch, actually had the chance to flight-test the Me 163 aircraft. At least one aircraft was still operational by February 1945 and was used for testing the 55 mm R4M rockets by Erprobungkommando 16.

Me 163A at Peenemunde, 1943. [Ransom & Cammann]
At least one Me 163A survived up to February 1945. It was used by Erprobungkommando 16 (Eng. testing or evaluation-coomand) in Silesia to test the 55 mm R4M rockets. This unit had the primary function of testing and examining the newly built Me 163 and helping in the development and improvement of its overall design. Besides these, no other armament was installed on the Me 163 A series. Source Source: W. Spate and R. P. Bateson Messerschmitt Me 163 Komet

Technical Characteristics

The Me 163A was a high-speed, rocket-powered, swept-wing, short fuselage, mixed-construction tailless aircraft. The Me 163A fuselage was built using metal, divided into three sections, the front cockpit, central fuel tank, and the aft engine compartment.

The wooden wings had a very simple design consisting of two spars covered in thick fabric. If needed, the wings could be detached from the fuselage for transport. At the wings’ trailing edges ailerons were placed, which the pilot during flight used for pitch and roll. The wing area was 17.5 m² (57.4 ft²). The tail did not have the standard horizontal stabilizers, instead of having a single large vertical stabilizer. Despite this, no major problems during flights were ever noted on the Me 163A.

For the pilot to enter the cockpit he was provided with a ladder placed on the left side of the aircraft. The cockpit canopy opened upwards. Overall visibility was poor, and later versions would have an improved canopy. While it did offer some improvements for the pilot’s line of sight, it would not resolve the overall poor visibility of the aircraft. Given that the Me 163A was based on a DFS 194 glider, it was equipped with minimal instrumentation needed for the aircraft to be flown.

View of the Me 163A’s cockpit interior. [Spate & Bateson]
The Me 163A was powered by a single HWK R II 203 rocket engine, which gave 750 kg (1,650 lb) of thrust. The main fuel consisted of a mix of T and Z Stoff. These two chemicals were highly reactive, volatile, and prone to explosion. To avoid this, extensive preparation and security measures were necessary. The maximum speed this engine achieved was some 850 km/h (530 mph). This high speed was achieved to some extent thanks to the aircraft’s low weight. The empty weight was 1,140 kg (2,513 lbs) while the maximum takeoff weight was 2,200 kg (4,850 lbs).

Interestingly, in order to save weight, the Me 163 did not have a conventional landing gear unit. Instead, during take-off, it was provided with a specially designed two-wheel dolly. It would be jettisoned upon take-off. When landing on the airfield, the Me 163 used a retractable skid located beneath the fuselage.

Despite the A series having not been designed to have any weapon systems, at least one Me 163A was tested with the installation of the 5.5 cm (2.16 in) R4M air-to-air rockets.

Production Versions

  • DSF 194 – Prototype whose further development led to the creation of the Me 163
  • Me 163 Prototype Series– Prototype aircraft
  • Me 163A-0 – 10 Pre-production aircraft built

Conclusion

The Me 163A series, despite its unusual appearance and overall design, proved to be a rather successful aircraft. It had some shortcomings, mostly regarding its dangerous fuel load. Upon completion of successful testing, order for the Me 163B version was given.

Me 163A Specifications

Wingspans 8.85 m / 29 ft 3 in
Length 5.25 m / 17 ft 2 in
Height 2.16 m / 7 ft 8 in
Wing Area 17.5 m² / 57.4 ft²
Engine One HWK R II 203 rocket engine with 750 kg (1,650 lbs) of thrust
Empty Weight 1,140 kg / 2,513 lbs
Maximum Takeoff Weight 2,200 kg / 4,850 lbs
Maximum Speed 850 km/h / 530 mph
Crew 1 pilot

Gallery

Me 163A – Illustrated by Carpaticus

Credits

  • Written by Marko P.
  • Edited by by Ed Jackson & Henry H.
  • Illustrations by Carpaticus

Sources

  • D. Nešić (2008) Naoružanje Drugog Svetsko Rata-Nemcaka. Beograd.
  • W. Spate and R. P. Bateson (1971) Messerschmitt Me 163 Komet , Profile Publications
  • M. Ziegler (1990) Messerschmitt Me 163 Komet, Schiffer Publishing
  • M. Emmerling and J. Dressel (1992) Messerschmitt Me 163 “Komet” Vol.II, Schiffer Military History
  • E. T. Maloney and U. Feist (1968) Messerschmitt Me 163, Fallbrook
  • S. Ransom and H.H. Cammann (2010) Jagdgeschwader 400, Osprey publishing.
  • D. Donald (1990) German aircraft of the WWII, Brown Packaging books ltd
  • D. Monday (2006) The Hamlyn Concise Guide To Axis Aircraft OF World War II, Bounty Books.
  • M. Griehl (1998) Jet Planes of the Third Reich, Monogram Aviation Publication
  • M. Griehl (2012) X-Planes German Luftwaffe Prototypes 1930-1945, Frontline Book
Linke Hofmann R.8/15

Linke-Hofmann R.I

German Empire Flag German Empire (1917)
Heavy Bomber Prototype- 4 Built

Linke-Hoffman R.I 40/16 side view. [The German Giants]
The Linke-Hofmann R.I was an experimental heavy bomber developed by the German Empire in 1917. The R.I would be unique, as one of the first prototypes to be constructed mostly out of a translucent material known as cellon, with the idea that it aircraft would be harder to spot. Unfortunately for the designers, cellon is highly reflective and ended up making the craft a much more noticeable target. After the failure with cellon, more work continued on the prototypes, now of normal fabric skinned construction. Due to poor performance caused by several design choices, the type was not mass produced and was subsequently cancelled.

History

A drawing of the R.I done by Linke-Hoffman. Notice the 3 gun positions. [German Aircraft of Minor Manufacturers Volume II]
During times of war, it is not too uncommon for companies, factories and other industrial firms to be drawn into the war effort and end up producing materials that are as far away from their specialty as possible. Sometimes, this can end in a surprise success or a total blunder. This was no exception in the first World War for the German Empire. The concept of the military airplane had seen its first successes early in the war,and the need for aircraft was on the rise, but a major problem came in the fact that there were few dedicated airplane companies in Germany at the time. Thus, the Empire would call upon many of its industrial manufacturers to begin designing and producing aircraft, even if they were not familiar with working in that field. Linke-Hofmannn would be one such company.

3-Way drawing of both versions of the R.I [The German Giants]
Linke-Hofmann, sometimes misspelled Linke-Hoffman, was founded in 1912 and was a manufacturer of railroad components, mainly locomotives and rolling stock. In early 1916, the company would enter the field of aviation by using their factories for aircraft repairs and for license built construction of aircraft. Some aircraft types they built under license were the Roland C.IIa, Albatros C.III, Albatros C.X and the Albatros B.IIa. At the same time, Linke-Hofmann was also awarded a contract to produce their own aircraft. The first of their home built aircraft would be an R-Plane type or Riesenflugzeug (giant aircraft), which was the designation given to the largest multi-engine bomber aircraft of the Empire. Linke-Hofmann’s R.I design would be a strange looking machine. Its fuselage was short and tear-drop shaped to streamline the design . Each pair of wings would be mounted extremely high and low on the fuselage in an attempt to increase lift. Four internal engines would be connected to four propellers, two in pusher configuration and two in puller configuration. Most interestingly, a majority of the tail of the aircraft would be made out of a material called Cellon. Cellon (Cellulose Acetate) is a translucent, plant-based material similar to film that was tested on several German aircraft in WWI, swapping out the normal fabric. The idea behind having the airframe covered in such material was that it was thought to make the aircraft harder to see. In addition to the Cellon, the R.I also had a very large cockpit with a number of windows to give much better visibility. Many of these design choices were made as it was thought they would make the design perform better in the long run, but they would ultimately lead to its downfall.

The R.I 8/15 under construction. The Cellon is clearly visible [German Aircraft of Minor Manufacturers Volume II]
The Cellon tail of 8/15 [German Aircraft of Minor Manufacturers Volume II]

The completed R.I 8/15

Work began on the first R.I in the later months of 1916 under Chief Engineer Paul Stumpf, who previously worked for the AEG aircraft works. The first R.I was completed in early January of 1917 and was named the R.I 8/15. Testing of the aircraft began, but its first flight was delayed due to the unconventional steel tires coming apart during taxiing attempts. Improved versions of the tires were built that were much more stable than the first. Shortly after, the R.I 8/15 would fly for the first time from the Hundsfeld Airfield near Breslau, but the exact date is unknown. Early test flights showed the design was flawed and as time went on, performance began to suffer, although the exact reason was not known. Noticeably, the wings seemed to be the root cause of the lag in performance. The aircraft’s controls would occasionally become heavy and unresponsive, resulting in a partial loss of control. To amend this to some degree, several additional struts were added to the main wings, but this would not save the aircraft from disaster. On May 10th 1917, during its 6th test flight, two of the wings on the R.I 8/15 would collapse mid-flight and the aircraft would slam into the ground at full speed. Remarkably, all of the crew of the aircraft would survive, but the airframe itself would be destroyed in a blaze of fire caused by the crash. Unfortunately, 1-2 ground crew would die from the flames while trying to put them out.

The destruction of the 8/15 would force Linke-Hofmann to look into designing an improved model. At this time, many of the design choices Linke-Hofmann made with the aircraft would show how ineffective and even detrimental they were. The wings themselves were the root cause of the crash, as they were not stable nor very well supported. The Cellon material, which was thought to make the aircraft invisible, actually ended up doing the exact opposite, as the material was highly reflective, especially while the aircraft was airborne. Cellon itself also was not the most stable material to make most of the tail section of the aircraft out of, as the material itself could easily bend and warp during rough weather. Even when the material worked as needed, it aged to a yellow color that would remove the translucency. Even before the aircraft took flight, Linke-Hofmann would be criticized for making an aircraft mostly out of the little tested material. In order to amend these issues, the Idflieg ,,the Imperial organization that handled aircraft development, ordered several improved models to continue the development of the type, as the 8/15 had crashed before most of the evaluation had completed. Linke-Hofmann would then begin construction on the improved models, serial numbers 40/16 through 42/16. These improved variants on the R.I attempted to fix many of the issues that plagued the 8/15. The wing structure was redesigned to be significantly more stable, with additional struts forming an overall better design. Most of the Cellon in the aircraft had been replaced with standard fabric, with only a few small patches of the tail containing it, likely to serve as observation windows. The landing gear was also heavily improved, something the Linke-Hofmann Engineers were quite proud of. Lastly, the new airframe was also built to accommodate three positions for machine gunners. These small improvements mended these few issues, but the aircraft’s design was still riddled with flaws.

40/16 in flight. [German Aircraft of Minor Manufacturers Volume II]
Details regarding the history of the improved variants are, unfortunately, not well known. It is unknown exactly when the R.I 40/16 first flew or when it was even built, but the handling of the aircraft had been significantly improved upon over the 8/15. Maneuverability was especially stated to be superb compared to the older model, but its general performance was still considered to be unsatisfactory. Landing the aircraft was stated to be terrible due to the high location of the pilot and the slow landing speed.

The crashed 40/16 after a taxiing accident. [German Aircraft of Minor Manufacturers Volume II]
During one landing attempt while testing the 40/16, the test pilot misjudged how close he was from the landing strip due to the height of the aircraft and damaged the landing gear. Due to the teardrop shape of the aircraft, the entire thing went nose down into the ground, crushing the entire cockpit section. It is unknown if anyone was killed or injured during the crash, but no attempt was made to repair the aircraft afterwards and it was likely scrapped. Details on the 41/16 and 42/16 are even more lacking. Some sources claim they were never completed, while other sources state they were complete and ready for inspection before the program concluded. 41/16, in particular, has virtually no information or photos of the aircraft, but two photos exist of a finished 42/16 sitting outside the Linke-Hofmann factory in Breslau.

Design

A direct frontal view of 40/16. The unique engine-propeller arrangement can be seen clearly, as well as the tall profile of the aircraft. [German Aircraft of Minor Manufacturers Volume II]
Pilot’s position of the R.I [German Aircraft of Minor Manufacturers Volume II]
The Linke-Hofmann R.I was a four engined R-Type aircraft with a large teardrop-shaped fuselage covered in fabric. The fuselage was designed in such a “whale” configuration to contain its engines and reduce drag, but this was only ever tested on smaller aircraft and likely detrimentally affected the R.I. The front of the aircraft was divided into three different floors. The first floor contained the pilot’s position and the wireless station for communication. This floor had extensive glasswork to provide a good view around the front of the aircraft. The large amount of glass used in the cockpit only helped during clear weather as, during rain or if illuminated by a searchlight, it would cause visibility to suffer from light reflection and condensation.

Engine Room containing the four Mercedes D.IVa engines

The second floor contained the four Mercedes D.IVa engines. The third and lowest level contained the bombardier’s station and four internal fuel tanks. The tail of the R.I differed between the two variants. On the earlier 8/15, the tail was composed mostly of Cellon, while on the later 40/16, it was covered in fabric. The tail of the aircraft had a biplane horizontal stabilizer and three vertical fins for vertical stabilizers. The two additional fins vertically and the upper wing of the horizontal stabilizers were used as control surfaces on top of the conventional placement of said control surfaces. The wings of the aircraft were placed high and low on the aircraft, with the fuselage height directly separating each wing. Only the upper wings had ailerons fitted. The wings on the 8/15 were actually the lightest of any R-Plane built, which was a likely factor in its crash. The 40/16 had improved and more stabilized wings compared to its predecessor. The aircraft originally was planned to have four propellers, two in tractor and two in puller configuration but this design aspect doesn’t appear to have ever left the drawing board. Instead, only two were used in tractor layout. The engines powered the propellers in a very unique way. Each side of the aircraft had one propeller, which was connected to a pair of engines via outrigger frames and powered through a drive shaft connected to a bevel gear. Each pair of engines powered one side. This was done so that, in the event one of the engines was disabled through either malfunction or combat, the propellers would still have power going to them. A disabled propeller would begin windmilling, or rotating without power, and cause significant drag. On larger aircraft, this would seriously alter performance and cause the aircraft to lose speed and airflow due to drag. This complex system was put into place to prevent this from happening.

R.I 40/16 outside of the Linke-Hofmann factory. [The German Giants]
No armament was carried aboard the R.I, but several proposals were made. Three machine-guns of unknown type and caliber were to be located at three positions around the aircraft. Two were located on the tallest point of the body, with one facing forward and one facing backward to cover all angles. The third gun position was located in the middle of the aircraft, with two open windows on each side to provide maximum firing range to each side. Given it was an R-Plane, the R.I would have used bombs had it entered mass production, but it’s loadout was never addressed, since the type was considered a failure.

Conclusion

The only two images of the Linke-Hoffman R.I 42/16 near the Linke-Hoffman factory [The German Giants]
With the destruction of two aircraft and the type severely underperforming to expectations, the Idflieg lost their faith in Linke-Hofmann’s R.I program and it was promptly cancelled before January 1918. The 41/16 and 42/16 were most likely scrapped before the end of the war. The type was riddled with flaws from the beginning due to the strange decisions made by Linke-Hofmann in designing their first aircraft. Despite their failure at the start of their aircraft manufacturing career, Linke-Hofmann would use the experience learned from the R.I to create an improved and much more traditional looking R-Plane aircraft, the R.II.

Variants

  • Linke Hofmann R.I 8/15 – First version of the R.I. This version’s tail and rear fuselage were constructed of the transparent material Cellon.
  • Linke Hofmann R.I 40/16 – Improved version of the R.I 8/15. This type had many slight modifications, such as a better wing structure, a more stable landing gear, and was no longer constructed of Cellon. 3 of this type were built.

Operators

  • German Empire – The Linke-Hofmann R.I was an R-type aircraft meant to be used in the heavy bomber role for the German Empire. However, due to poor performance, the type was never mass produced or sent into service.

Linke-Hofmann R.I 40/16 Specifications

Wingspan 108 ft 11 in / 33.2 m
Upper Chord 16 ft 5 in / 5 m
Lower Chord 15 ft 5 in / 4.7 m
Length 51 ft 2 in / 15.6  m
Height 22 ft / 6.7 m
Wing Area 2851 ft² / 265 m²
Engine 4x 260 hp ( 193.9 kW ) Mercedes D.IVa engines
Weights
Empty 17,640 lb / 8,000 kg
Loaded 24,969 lb / 11,200 kg
Climb Rate
Time to 9,840 ft / 3,000 m 2 Hrs
Maximum Speed 81.8 mph / 130 km/h 
Crew 4-5 crewmen
Armament
  • 3x planned machine guns of unknown type.

 

Gallery

Illustrations by Ed Jackson

The Linke Hofmann R.8/15 – Note the extensive use of transparent cellon for the aft portion of the fuselage.
The Linke Hofmann R.40/16
3-Way drawing of both versions of the R.I [The German Giants]

Credits

  • Written by: Medicman11
  • Edited by: Stan L. & Henry H.
  • Illustrations by Ed Jackson

Sources

  • Kosin, Rüdiger. The German fighter since 1915. Baltimore, Md: Nautical & Aviation Pub. Co. of America, 1988. Print.
  • Herris, Jack. German Aircraft of Minor Manufacturers In WWI Volume 2: Krieger To Union, Columbia, SC: Aeronaut Books, 2020. Print.
  • Haddow, G. W., and Peter M. Grosz. The German giants : the German R-planes, 1914-1918. London: Putnam, 1988. Print.