Loening XFL: Difference between revisions
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{|{{Infobox Aircraft Begin |
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|name=XFL |
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|image= |
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|type=[[Fighter aircraft|Fighter]] |
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| type=fighter |
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|national origin=[[United States]] |
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|manufacturer=[[Loening Aeronautical Engineering]] |
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|designer= |
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|first flight=Never flew<ref name="Angel">Angelucci, 1987. pp. 292-293.</ref> |
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|retired= |
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|status=Never built |
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The '''Loening XFL''' was a proposed carrier |
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.<ref name="Angel"/> |
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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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|swept area sqm=<!-- swing-wings --> |
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|swept area sqft=<!-- swing-wings --> |
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|rot area sqm=<!-- helicopters --> |
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|rot area sqft=<!-- helicopters --> |
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|volume m3=<!-- lighter-than-air --> |
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|volume ft3=<!-- lighter-than-air --> |
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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=<!-- prop engines --> |
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|eng1 hp=625 |
|eng1 hp=625 |
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|eng2 number= |
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|eng2 type= |
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|eng2 kw=<!-- prop engines --> |
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|eng2 hp=<!-- prop engines --> |
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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=<!-- if max speed unknown --> |
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|cruise speed mph=<!-- if max speed unknown --> |
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|stall speed kmh=<!-- aerobatic and STOL aircraft --> |
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|stall speed mph=<!-- aerobatic and STOL aircraft --> |
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|range km= |
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|endurance h=<!-- if range unknown --> |
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|endurance min=<!-- if range unknown --> |
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|ceiling m= |
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|ceiling ft= |
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|g limits=<!-- aerobatic aircraft --> |
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|roll rate=<!-- aerobatic aircraft --> |
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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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|armament3= |
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|armament4= |
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|armament5= |
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|armament6= |
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}} |
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<!-- ==See also== --> |
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|see also= |
|see also= |
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|related= |
|related= |
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|similar aircraft= |
|similar aircraft= |
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|lists= |
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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 }} |
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<!-- ==External links== --> |
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{{Loening aircraft}} |
{{Loening aircraft}} |
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{{USN fighters}} |
{{USN fighters}} |
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{{Aviation lists}} |
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[[Category:United States fighter aircraft |
[[Category:1930s United States fighter aircraft|Loening FL]] |
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[[Category:Loening aircraft]] |
[[Category:Loening aircraft]] |
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{{aero-1930s-stub}} |
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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.
 | This aircraft of the 1930s article is a stub. You can help Wikipedia by expanding it. |