Loening XFL: Difference between revisions
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==Specifications (as designed)== |
==Specifications (as designed)== |
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{{Aircraft specs |
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{{aerospecs |
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|ref=Angelucci, 1987. pp. 292-293.<ref name="Angel"/> |
|ref=Angelucci, 1987. pp. 292-293.<ref name="Angel"/> |
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|prime units? = imp |
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|met or eng?=eng |
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|crew=1 |
|crew=1 |
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|capacity= |
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|length m=6.32 |
|length m=6.32 |
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|length ft=20 |
|length ft=20 |
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|span ft=28 |
|span ft=28 |
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|span in=0 |
|span in=0 |
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|height m= |
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|height ft= |
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|height in= |
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|wing area sqm= |
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|wing area sqft= |
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|empty weight kg=1,928 |
|empty weight kg=1,928 |
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|empty weight lb=4,250 |
|empty weight lb=4,250 |
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|gross weight kg= |
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|gross weight lb= |
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|eng1 number=1 |
|eng1 number=1 |
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|eng1 |
|eng1 name=[[Wright XR-1510]]-26 |
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|eng1 kw= |
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|eng1 hp=625 |
|eng1 hp=625 |
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|max speed kmh=322 |
|max speed kmh=322 |
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|max speed mph=200 |
|max speed mph=200 |
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|cruise speed kmh= |
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|cruise speed mph= |
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|stall speed kmh= |
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|stall speed mph= |
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|range km= |
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|range miles= |
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|endurance h= |
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|endurance min= |
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|ceiling m= |
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|ceiling ft= |
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|climb rate ms= |
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|climb rate ftmin= |
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|armament1= |
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|armament2= |
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}} |
}} |
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===Bibliography=== |
===Bibliography=== |
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*{{cite book |last= Angelucci |first= Enzo |title=The American Fighter from 1917 to the present |year=1987 |publisher=Orion Books |location=New York |
*{{cite book |last= Angelucci |first= Enzo |title=The American Fighter from 1917 to the present |year=1987 |publisher=Orion Books |location=New York }} |
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{{Loening aircraft}} |
{{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.
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