Loening XFL: Difference between revisions
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==Specifications (as designed)==
{{Aircraft specs
|ref=Angelucci, 1987. pp. 292-293.<ref name="Angel"/>
|prime units? = imp
|crew=1
|length m=6.32
|length ft=20
Line 34 ⟶ 33:
|span ft=28
|span in=0
|empty weight kg=1,928
|empty weight lb=4,250
|eng1 number=1
|eng1
|eng1 hp=625
|max speed kmh=322
|max speed mph=200
}}
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===Bibliography===
*{{cite book |last= Angelucci |first= Enzo |title=The American Fighter from 1917 to the present |year=1987 |publisher=Orion Books |location=New York
{{Loening aircraft}}
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Latest revision as of 06:02, 17 December 2020
XFL | |
---|---|
Role | Fighter |
National origin | United States |
Manufacturer | Loening Aeronautical Engineering |
First flight | Never flew[1] |
Status | Never built |
The Loening XFL was a proposed carrier-based fighter aircraft to be built by Loening Aeronautical Engineering for the US Navy. It won a 1933 competition, but Loening was already busy building other aircraft, so the contract was canceled.[1]
Specifications (as designed)[edit]
Data from Angelucci, 1987. pp. 292-293.[1]
General characteristics
- Crew: 1
- Length: 20 ft 9 in (6.32 m)
- Wingspan: 28 ft 0 in (8.53 m)
- Empty weight: 4,250 lb (1,928 kg)
- Powerplant: 1 × Wright XR-1510-26 , 625 hp (466 kW)
Performance
- Maximum speed: 200 mph (322 km/h, 170 kn)
References[edit]
Bibliography[edit]
- Angelucci, Enzo (1987). The American Fighter from 1917 to the present. New York: Orion Books.