Loening PW-2

Loening PW-2

__NOTOC__ Infobox Aircraft
name=Loening PW-2


caption=
type=Monoplane fighter
national origin=United States
manufacturer=Loening Aeronautical Engineering
designer=Grover Loening
first flight=1920
introduced=
retired=
status=
primary user=United States Army Air Corps
more users=
produced=
number built=7
developed from=Loening M-8
variants with their own articles=
The Leoning PW-2 was a 1920s American single-seat fighter monoplane designed by Grover Loening and built by his Loening Aeronautical Engineering Company.

Development

Based on the earlier two-seat braced-wing monoplane fighter the M-8 the PW-2 was a single-seat variant for the United States Army Air Corps. It had a fixed tailskid landing gear and was powered by a nose-mounted Wright-Hispano H engine with a tractor propeller. The pilot had an open cockpit. The company built three prototypes designated the PW-2 and a production order for ten aircraft designated the PW-2A followed. The PW-2As were similar to the PW-2 but had a revised tail unit. After four aircraft had been delivered, one aircraft crashed when the wings separated from the aircraft; the contract was canceled. One of the PW-2As was modified with shorter-span wings and a 350hp (261kW) Packard 1A-1237 engine as the PW-2B.

Variants

;PW-2:Prototype, three built one of which had twin rudders and was not flown and used for static testing.;PW-2A:Production variant with revised tail unit, four built and six cancelled.;PW-2B:One PW-2A modified with shorter span wings and a 350hp (261kW) Packard 1A-1237

Operators

;USA:United States Army Air Corps

pecifications (PW-2A)

aerospecs
ref=Fighters of the United States Air Force Dorr and Donald 1990, p.25.]
met or eng?= eng

crew=1
capacity=
length m=7.95
length ft=26
length in=1
span m=12.12
span ft=39
span in=9
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=
height ft=
height in=
wing area sqm=27.8
wing area sqft=299 Swanborough and Bowers 1962, p.519.]
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=1270
gross weight lb=2799
lift kg=
lift lb=

eng1 number=1
eng1 type=Wright-Hispano H engine
eng1 kw= 239
eng1 hp= 320
eng1 kn=
eng1 lbf=
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=219
max speed mph=136
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=

armament1=Twin 0.3in (7.62mm) Lewis machine gun
armament2=
armament3=
armament4=
armament5=
armament6=

ee also

aircontent
see also=
related=
* Loening M-8
similar aircraft=
sequence=
lists=
* List of military aircraft of the United States

References

Notes

Bibliography

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*
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*cite book |last= |first= |authorlink= |coauthors= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|year= |publisher= Orbis Publishing|location= |issn=|pages=2376


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