/Airplanes/Axis/Germany/01-Fighters/Me-P1101/Data/Me-P1101.htm | Update: -

 

Messerschmitt Me P.1101

GENERAL DATA
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Fighter
 
Messerschmitt
1 unfinished prototype
Never flown
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Variants
The 24 July 1944 design by Hans Hornung of a single-seat jet fighter. It was powered by one Heinkel He S 011 turbojet. This was the shortest of all versions with a blunt nose and a v-tail. It had a wingspan of 7.15 m and a length of 6.85 m. The armament was two MK 108 cannon.
A sleeker design, dating from 30 August 1944. Also a v-tailed single-seat jet fighter with a more pointed nose and wings swept back at 40 degrees. It had a wingspan of 8.16 m and a length of 9.37 m.[
Full-scale prototype design of a flying test single-seat jet fighter with a wingspan of 8.06 m and a length of 8.98 m. It had a conventional tail and swept wings designed to be set at different angles while on the ground. Test flights were first intended to be undertaken with a 35-degree wing sweep, followed by a 45-degree sweep. The first test flight was to take place in June 1945.[
The final single-seat jet fighter design that went into production with a wingspan of 8.25 m, a length of 9.175 m and a weight of 1250 kg.
A ramjet-powered single-seat fighter that would have eight additional small rocket engines for takeoff. This design would have a much wider fuselage covering the large Lorin ramjet located to the back of the cockpit, as well as a conventional tail.
A different design of a two-seat v-tailed heavy fighter and destroyer. It was an all-metal aircraft armed with a large 7.5 cm Pak 40 cannon and was powered by two Heinkel He S 011 turbojets. It had a wingspan of 13.28 m and a length of 13.1 m.
Another very different variant altogether. Two-seat attack/destroyer all-metal aircraft powered by four Heinkel He S 011 turbojets. It had the cockpit at the front end of the fuselage and was armed with a 7.5 cm Pak 40 cannon and one MK 112 55 mm autocannon in the nose, and four additional MK 112 in Schräge Musik configuration behind the cockpit. Its tail was of the conventional type and it had a wingspan of 15.4 m and a length of 15.2 m.


Fourth design 22 February 1945

DIMENSIONS
9.18 m
2594 kg
8.25 m
4065 kg
3.71 m
4500 kg
15.9 m²
296.5 kg/m²

ARMAMENT
4 × 30mm MK 108 cannons
4 x 53
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2-4 × Ruhrstahl X-4 air-to-air missiles
Radar FuG 15 et FuG 25a

 

POWERPLANT
1 × Heinkel HeS 011A turbojet engine
12.07 kN thrust
?
1432 L (internal) + 500 L drop tank

 

PERFORMANCES
980 km/h at 7000 m (estimated)
905 km/h
170 km/h
14000 m
22.2 m/s
1500 km

(*) vitesse de décrochage

Sources

 

Drawings

 

 

 

Fighters