Messerschmitt Me 163C

Nazi flag Nazi Germany (1944)

Rocket-Powered Interceptor Fighter: Reached Prototyping Stage

A diagram of the improved rocket interceptor. (Nevingtonwarmuseum)

When the Me 163B entered service, it was a unique aircraft by virtue of its rocket engine. It was used as a short range interceptor for German air defense, and while it could achieve extremely high speeds, its overall design left much to be desired. These faults included a highly restrictive view from the cockpit, a lack of retractable landing gear, and limited operational endurance. In order to address some of these issues,  Messerschmitt engineers developed the Me 163C.

 

History 

While the Me 163B Komet proved to be a remarkable design, it was quite dangerous to fly  and there was plenty of room for improvement.  In order to make the whole aircraft as cheap as possible, some limitations had been introduced. To save weight, the aircraft had rather small dimensions which, in turn, limited the fuel load that could be stored inside. This led to a limited powered flight time of fewer than 8 minutes. In combat operations, this proved to be insufficient, but there was little that the German engineers could do to improve this. Adding internal or external auxiliary fuel tanks was not possible given the design restrictions.

Me 163B rocket interceptor, accepted into limited service. (militaryimages.net)

The position and layout of the cockpit also offered a number of issues. Most importantly, it provided the pilot with a limited field of view behind his aircraft. Another issue was the lack of retractable landing gear. The Me 163 was instead forced to use a two-wheeled detachable dolly. This was intentionally done in order to reduce weight.

Once the aircraft was in the air, the dolly was jettisoned. 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 landing, the Me 163 was to use a simple retractable landing skid, placed beneath the fuselage. After landing, the aircraft was immobile and became an easy target for enemy fighters. For this reason, a normal retracting landing gear unit was desirable, but once again for the same reason as the fuel load, this could not be implemented.

To redress the previously mentioned issues, engineers at Messerschmitt began working on an improved version, the Me 163C. It incorporated a longer fuselage, an improved cockpit, and had an engine with two combustion chambers. The development of this version likely started in late 1944 or early 1945.

Production and service

The precise development history, and how many aircraft of this version were built, are the subject of considerable speculation. The fact that there are no photographs of it complicates the matter further. Most sources mentioned that only a few incomplete airframes were built by the Germans. In some sources, for example B. Rose’s Secret Projects Flying Wings and Tailless Aircraft, it is mentioned that three prototypes were completed and flight-tested in early 1945.  Source E. T. Maloney and U. Feist on the other hand, mentions that only a few pre-prototype airframes were built by the time the war ended in Europe. So there are two completely different accounts in the sources.

Technical characteristics

The Me 163C, 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 version, with its fuselage being built of metal, and possessing wooden wings. The semi-monocoque fuselage was longer and was now 7 m compared to the original 5.84 m length.

The Me 163C was to be powered by an improved Walter 109-509C or an HWK 109-509A-2 rocket engine. In the case of the first engine, it could generate a thrust of some 1.500 kg.  An auxiliary HWK 509 rocket engine would be used to provide additional endurance once the aircraft reached its cruising altitude. The maximum speed of the Me 163C was estimated at 915 km/h while the operational range was 125 km.

While the introduction of retractable landing gear was desirable, the Me 163C was not to be equipped with one, but it still received some modifications in this regard. It was to have a fully retractable tail wheel located at the bottom of the tail assembly.

The cockpit was completely redesigned. It received a fully glazed bubble-type canopy. This offered the pilot a much improved all-around view. In addition, there were provisions for pressurization equipment.

The armament used on this aircraft is not quite clear in the sources. It would have consisted of either two 2 cm MG 151 with 100 rounds of ammunition for each cannon, two 30 mm MK108 cannons with 60 rounds, or less realistically, four 30 mm MK108 cannons with 40 rounds of ammunition.

Note the redesigned canopy, auxiliary engine, and extended fuselage. (www.walterwerke.co.uk)

Cancelation of the project

While the precise development of this aircraft is unclear, most sources agree on the reasons why it was not adopted, beyond the obvious end of the war. Basically, there were two main reasons for this. First, was the lack of landing gear. The Me 163C still had to take off and land using the take-off dolly and the landing skid. This was far from perfect as the dolly, as mentioned, could potentially damage the aircraft itself after release, and the use of a sliding skid made the aircraft immobile after landing. Lastly, the auxiliary engine only extended the operational flight by an additional 1-minute, which was deemed insufficient.  It was for these reasons that  the Me 163C would not be adopted, and instead the development of the much improved Me 163D was prioritized.

Conclusion

Given its experimental nature, it’s late introduction, and the disagreement between sources, it is quite difficult to make the final decision on the general properties of this aircraft. Given that the project was canceled by the Germans, it is likely that besides a few experimental prototypes, no actual production aircraft were be assembled. Regardless it served as a stepping stone for the next version, the Me 163D, which was built, but it too would not be adopted for service due to the end of the war.

Me 163C Specifications

Wingspans 32 ft 2 in / 9.8 m
Length 23 ft 1 in / 7 m
Height 3 m / ft  in
Wing Area 220 ft² /  20.41 m²
Engine Walther HWL 509C-1 liquid fuel  rocket engine with a max thrust of 1.500 kg
Empty Weight 4,850 lbs / 2,200 kg
Maximum Takeoff Weight 11,680 lbs / 5.300 kg
Maximum Speed 570 mph / 915 km/h
Operational range 78 mil / 125 km
Engine endurance 12 minutes
Maximum Service Ceiling 40,000 ft /  12,200 m
Crew One pilot
Armament
  • Two 20 cm MG 151 (100) / Two 30 mm MK108 cannons  60
The Me 163C Rocket powered interceptor.

Credits

  • Article written by Marko P.
  • Edited by  Henry H. and Medicman11
  • Ported by Marko P.
  • Illustrations 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, Putnam
  • 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
  • B. Rose (2010) Secret Projects Flying Wings and Tailless Aircraft, Midland
  • http://www.walterwerke.co.uk/walter/me163d.htm

 

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