- Gallaudet PW-4
The Gallaudet PW-4 was a prototype biplane fighter aircraft built by the
Gallaudet Aircraft Company . It was one of the last projects by the company before it was taken over byConsolidated Aircraft . It was all metal, powered by aPackard 11A-1237 engine. Three prototypes were ordered by theUSAAC , but the company could only afford to build 1, which never flew.pecifications
aerospecs
ref=Angelucci, 1987. pp. 202-203.
met or eng?=engcrew=1
capacity=
length m=6.90
length ft=22
length in=8
span m=9.09
span ft=29
span in=10
height m=2.43
height ft=8
height in=0
wing area sqm=22.76
wing area sqft=245
empty weight kg=999
empty weight lb=2,203
gross weight kg=1,379
gross weight lb=3,040eng1 number=1
eng1 type=Packard 1A-1237
eng1 kw= 260
eng1 hp=350
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=max speed kmh=233
max speed mph=145
cruise speed kmh=
cruise speed mph=
stall speed kmh=
stall speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=
ceiling ft=
g limits=
roll rate=
climb rate ms=
climb rate ftmin=armament1=
armament2=
armament3=
armament4=
armament5=
armament6=aircontent
see also=
related=
similar aircraft=
lists=References
Bibliography
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