- Focke-Wulf Project II
__NOTOC__ Infobox Aircraft
name=Project II
caption=
type=Fighter
manufacturer=Focke-Wulf
designer=
first flight=
introduced=
retired=
status=Abandoned design study
primary user=
more users=
produced=
number built=
variants with their own articles=The Focke-Wulf Project II was a design study for a jet fighter carried out in Germany during World War II. Due to the manufacturing difficulties were envisaged with other all-new jet fighter developments, Focke-Wulf's second design was nothing more than a development of the
Focke-Wulf Fw 190 , but powered with a jet engine, positioned on a redesigned fuselage. This engine, aJumo 004 , was to be housed beneath the nose. A conventional undercarriage was used. The low position of the jet intake raised the likelihood of foreign bodies being sucked up and in any case, the engine would burn the runway. This design development ceased in March 1943.pecifications (as designed)
aerospecs
met or eng?= metcrew=one pilot
capacity=
length m=9.85
length ft=32
length in=4
span m=9.70
span ft=31
span in=10
dia m=
dia ft=
dia in=
height m=
height ft=
height in=
wing area sqm=15.0
wing area sqft=161
rot area sqm=
rot area sqft=
aspect ratio=
empty weight kg=2,410
empty weight lb=5,313
gross weight kg=3,350
gross weight lb=7,385eng1 number=1
eng1 type=Junkers Jumo 004 B
eng1 kw=
eng1 hp=
eng1 kn= 8.7
eng1 lbf= 1,962
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
eng2 lbf-ab=max speed kmh=825
max speed mph=515
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=640
range miles=397
endurance h=
endurance min=
ceiling m=12,400
ceiling ft=40,600
glide ratio=
climb rate ms=20
climb rate ftmin=4,000
sink rate ms=
sink rate ftmin=armament1=2 × 30 mm
MK 108 cannon s
armament2=2 × 20 mmMG 151 machine gun s
armament3=
armament4=
armament5=
armament6=References
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similar aircraft=
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