Grumman XP-50

· Grumman

Airplanes

Length

9.73 m

Flat Wing Span

12.8 m

Height

3.66 m

Flat Wing Area

28.24 m²

Max Speed

680 km/h

Max Ceiling

12190 m

Number of Engines

First Flight

1941-02-18

Number Built

Maximum Take-Off Weight

6.53 t (paragliders: kg)

Maximum Range

2010 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Grumman XP-50	6.53	2010

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Romano R.110	Renault 12R	9.66	12.8		Compare
Tairov Ta-3	Tumansky M-88	9.827	12.658		Compare
Boulton Paul Bittern	Armstrong Siddeley Lynx	9.7536	12.4968		Compare
Short Scion	Pobjoy Niagara	9.4488	12.8016	6	Compare
Lippisch P.13		9.4	12.8		Compare
Messerschmitt Me 262		10.6	12.6		Compare

All data (19 fields)

Name: Grumman XP-50
Manufacturer: Grumman
Description: The Grumman XP-50 was a land-based development of the shipboard XF5F-1 Skyrocket fighter, entered into a United States Army Air Corps (USAAC) contest for a twin-engine heavy interceptor aircraft.
First Flight: 1941-02-18
Designer: Grumman
Type: Heavy fighter; Interceptor
Length (m): 9.73
Height (m): 3.66
Max Speed (km/h): 680
Max Ceiling (m): 12190
Rate of Climb (m/s): 25
Armament: 2 × 20 mm (.79 in) cannons (60 rounds per gun); 2 × 0.50 in (12.7 mm) machine guns (500 rounds per gun); 2 × 100 lb (50 kg) bombs
Number Built: 1
Powerplant Description: 2 × Wright R-1820-67/69 9-cylinder air-cooled radial engines, 895 kW (1200 hp) each
Status: Cancelled
Wikipedia Article (URL): en.wikipedia.org/wiki/Grumman_XP-50
Flat Wing Span (m): 12.8
Flat Wing Area (m²): 28.24
Number of Engines: 2