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Submission declined on 11 March 2026 by Two pieces of toast (talk).
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| XP-65 | |
|---|---|
| General information | |
| Type | |
| Manufacturer | Grumman Aircraft Engineering Corporation |
| Status | Cancelled |
| Number built | 0 |
| History | |
| Developed from | XP-50 |
The Grumman XP-65 was a twin engine figther that was developed alongside the Navy's F7F Tigercat, but that was cancelled early in 1942 before it could reach the prototype stage.
With the loss of the XP-50 on 14 May 1941, the Army Air Corps transferred funding to the XP-65 project, that was originally named G-51.[1] It would have been an advanced version of the XP-50, using the more powerful Pratt & Whitney R-2800 Double Wasp air cooled eighteen cylinder radial engine.[2] It was to have thick mid mounted wings with a straight leading edge. The engines were to be carried in nacelles partly under the wings. The fuselage was to be narrow but tall with a oval cross section, with the cockpit just in front of the leading edge of the wing. It was to use tricycle landing gear.[3] Initially the hope was that the basic G-51 design could be used by the USAAC and the US Navy, needing only one production line. But it wasn't possible, so the main difference between the two versions was that the Army version would use turbo-superchargers. The Navy version would remove the superchargers, but would need arrestor hooks, folding wings. The Navy's version of the G-51 moved on to become the XF7F-1.[4]
Here is the corrected template filled with the XP-50 data you previously provided:
General characteristics
Performance
Armament
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