Tucker XP-57: Difference between revisions
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==Specifications (XP-57, proposed)== |
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[[Image:Tucker XP-57.jpg|right|300px|Orthographically projected diagram of the XP-57 proposal.]] |
[[Image:Tucker XP-57.jpg|right|300px|Orthographically projected diagram of the XP-57 proposal.]] |
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|max speed alt=495 km/h |
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|range main=960 mi |
|range main=960 mi |
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|range alt=600 km |
|range alt=600 km |
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|armament= |
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|related= |
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|similar aircraft= |
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* [[Bell XP-77]] |
* [[Bell XP-77]] |
Revision as of 04:26, 5 November 2009
P-57 | |
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Role | Fighter |
Manufacturer | Tucker |
Status | Cancelled |
Number built | None |
Tucker XP-57 was the designation of a lightweight fighter which was proposed to the United States Army Air Corps (USAAC) in 1940.
To minimize weight, the aircraft was to have a metal tubing frame with aluminum skin and plywood wings. The inline-8 engine was to sit behind the pilot in a configuration similar to the P-39 Airacobra. The USAAC ordered a single XP-57 prototype. However, when design was delayed due to financial problems in the company, the contract was allowed to lapse. No production aircraft was ever built because the USAAC was moving towards larger fighters and had lost interest in the project.
Specifications (XP-57, proposed)
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them. |
General characteristics
- Crew: 1
Performance
Armament
- 3x 0.50 cal (12.7 mm) machine guns or 1x 0.50 cal machine gun and 2x 20 mm cannons.
See also
Aircraft of comparable role, configuration, and era