Heinkel P. 1078
Heinkel P. 1078 | |
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Model of execution P.1078 B |
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Type: | Fighter plane |
Design country: | |
Manufacturer: | |
The project Heinkel P.1078 originated by tendering the OKL 1944 for a single-seat day fighter with Heinkel HeS-011 -Strahltriebwerk, four MK-108 - machine guns h and a required maximum speed of 1000 km /.
The basic version P.1078 A was planned as a conventional aircraft with swept wings. Like almost all designs of that time, this one also had a pressurized cabin with an ejection seat and an optional search radar in the nose. In addition, a P.1078 B with a completely different structure was developed. So this design was designed as a brushless aircraft with a double fuselage bow. The air inlet was in between.
In comparison, both variants were subject to the other drafts. The Junkers EF 128 won the tender .
Technical specifications
The following data was configured or calculated:
Parameter | Data (P 1078) | Data (P 1078 A) | Data (P 1078 B) |
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crew | 1 | ||
span | 9.0 m | 8.8 m | 9.4 m |
length | 6.10 m | ||
height | 2.35 m | ||
Wing area | 17.8 m² | 16.85 m² | 20.3 m² |
Wing extension | 4.55 | 4.6 | 4.35 |
Preparation mass | 2,454 kg | ||
Takeoff mass | 3,920 kg | 4,050 kg | 3,900 kg |
drive | a Heinkel HeS 011 jet engine | ||
power | 1,300 kp static thrust 1,035 kp near the ground at 900 km / h 445 kp at an altitude of 11,000 m at 900 km / h |
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Fuel volume | 1,200 kg | ||
Top speed | 1,025 km / h near the ground, 1,050 km / h at an altitude of 7,000 km |
980 km / h near the ground 955 km / h at an altitude of 6,000 m 890 km / h at an altitude of 11,000 m |
1,025 km near the ground 975 km / h at 6,000 km altitude 910 km / h at 11,000 km altitude |
Landing speed | 182 km / h | 160 km / h | 155 km / h |
Rate of climb | 29.8 m / s near the ground | 26.3 m / s near the ground, 16.8 m / s at a height of 6,000 m, 6.7 m / s at a height of 11,000 m |
29.8 m / s near the ground 19.8 m / s at a height of 6,000 m 9.5 m / s at a height of 11,000 m |
Rise time | 5.8 min at an altitude of 6,000 m 16.1 min at an altitude of 11,000 m |
4.9 min at an altitude of 6,000 m, 12.6 min at an altitude of 11,000 m |
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Flight route / duration | 580 km in 0.6 h near the ground 930 km in 1.0 h at 6,000 m altitude 1,500 km in 1.75 h at 11,000 m altitude |
580 km in 0.6 h near the ground 930 km in 1.0 h at 6,000 m altitude 1,550 km in 1.75 h at 11,000 m altitude |
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Service ceiling (1 m / s climb) |
12,900 m | 13,700 m | |
Take-off run | 700 m | 790 m 390 m with 1,000 kp start-up missiles |
730 m 360 m with 1,000 kp start-up missiles |
Landing runway | 640 m |
See also
literature
- Volker Koos: Heinkel rocket and jet aircraft . Aviatic, Oberhaching 2008, ISBN 978-3-925505-82-9 .
Web links
- www.luft46.com/Heinkel Note: References etc. are missing there, but the page appears to be at least well researched for the most part.