| 词条 | Focke-Wulf Project I | |||||||||||||||
| 释义 |
The Focke-Wulf Project I was a design study for a jet fighter, to be built in Germany during World War II. In 1942, the Reichsluftministerium (RLM) asked Professor Kurt Tank of the Focke-Wulf factory to investigate the possibility of a single-engine jet fighter. He was given the development plans of the BMW 003, Jumo 004 and Heinkel HeS 011 engines. Late in 1942 the Project Office, led by Ludwig Mittelhuber, began to work on a series of fighter projects, to be powered by one of these new turbojet units. The first proposed design featured a BMW P.330 2 or Jumo 004 engine, positioned on the fuselage back. The pilot was situated in the fuselage nose, and underneath were four units of armament. Its mid-wing was swept forward and the V-tail was swept back. The mainwheels of the tricycle undercarriage were so positioned under the fuselage that they could lie between themselves, when retracted. Specifications (as designed){{aerospecs|met or eng?=met |crew=one pilot |capacity= |length m=10.50 |length ft=34 |length in=5 |span m=8.20 |span ft=26 |span in=11 |height m= |height ft= |height in= |wing area sqm=14.0 |wing area sqft=151 |empty weight kg= |empty weight lb= |gross weight kg= |gross weight lb= |eng1 number=1 |eng1 type=BMW P.3302 turbojet |eng1 kn=5.9 |eng1 lbf=1,322 |eng1 kn-ab= |eng1 lbf-ab= |eng2 number= |eng2 type= |eng2 kn= |eng2 lbf= |eng2 kn-ab= |eng2 lbf-ab= |max speed kmh=800 |max speed mph=500 |cruise speed kmh= |cruise speed mph= |range km= |range miles= |endurance h=1 |endurance min=30 |ceiling m=10,800 |ceiling ft=35,500 |climb rate ms=11.0 |climb rate ftmin=2,165 |armament1=2 × 30 mm (1.18 in) MK 108 cannons |armament2=2 × 15 mm (.59 in) MG 151 cannons |armament3= |armament4= |armament5= |armament6= }} See also
|related= |similar aircraft= |sequence= I - II - III - IV - V - VI - VII - VIII|lists= |see also= }} References{{commons category|Focke-Wulf}}
5 : Abandoned military aircraft projects of Germany|Focke-Wulf aircraft|Single-engined jet aircraft|Forward-swept-wing aircraft|V-tail aircraft |
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