Messerschmitt Me 163 'Komet

Messerschmitt Me 163 'Komet'

The Messerschmitt Me 163A was as a research aircraft with rocket propulsion designed by Dr. Alexander M Lippisch.

Developed from the Me 163A was the Me 163B, A single seat target defense fighter. It featured a constant 22.3 degrees of wing sweepback at quarter chord, lacked horizontal tail surfaces and utilized a jettisonable twin-wheel dolly for take off and a retractable skid for landing.

A total of six prototypes and 70 pre-series were ordered. The first prototype (Me 163B V1) was completed in April 1942, but it had to wait for the completion of the first HWK R II-211 rocket motor for it's propulsion. The first flight with the rocket engine took place on June the 23rd 1943 (prototype Me 163B V2)

The HWK 509A-1 production rocket engine produced a max. thrust of 1700 kg for 7.5 minutes.

In May 1944 the Luftwaffe accepted it's first Me 163B, unofficially it was called 'Komet' a total of 279 Me163's were delivered, it was not very successful, 80 per cent suffered damage from take off or landing accidents and 15 per cent lost control in a dive or had fire onboard in the air.

Development of the Me 163C from the Me 163B with improved rocket engine that could last for 19 minutes started in January 1943, testing scheduled for August 1944 newer took place. No Me163C was ever completed or tested.

Developing Nation:	Germany
Manufacturer/designer:	Messerschmitt, by Dr. Alexander M Lippisch.
Task:	Single seat target defense fighter
First Flight:	Me 163B: June 23, 1943 Me 163C: Was being developed, never tested. first test were scheduled for August 1944.
First Delivery:	May 1944
First Operational:	May / June 1944
Crew:	1
Ejection Seat:	no
	Me 163B-1a
Wing Span:	9.33 m
Wing Area:	18.5 m²
Length:	5.85 m
Height: (on Dolly)	2.76 m
Engine (s):	HWK 509A-1
Weight:	1908 kg
Max. Take off weight:	4310 kg
Max. Speed:	955 Kph
Max. Range:	35.5 km
Weapons:	Two 20 mm MG 151 cannon's (Me 163Ba-1) Two 30 mm MK 108 cannon's (Me 163B-1a)

Research : M. van Leeuwen