United States (cancelled)
(OPERATORS list includes past, present, and future operators when applicable)
Width/Span
75.0 ft
(22.85 m)
MTOW
27,227 lb
(12,350 kg)
(Showcased structural values pertain to the base Vought VS-302 production variant)
Installed:
2 x Wright R-2600 air-cooled radial piston engines OR 2 x Pratt & Whitney R-2800 air-cooled radial piston engines of unknown output power each driving three-bladed propeller units.
Max Speed
351 mph
(565 kph | 305 kts)
Ceiling
35,597 ft
(10,850 m | 7 mi)
♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
(Showcased performance specifications pertain to the base Vought VS-302 production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
PROPOSED:
1 x Machine gun in nose position.
1 x Machine gun in left waist blister position.
1 x Machine gun in right waist blister position.
Internal bomb bay carrying between 2,000lb and 2,200lb of conventional drop bombs (1 x 2000lb; 2 x 1,000lb; 4 x 500lb; 20 x 100lb).
(Not all ordnance types may be represented in the showcase above)
VS-302 - Base Project Designation; project not selected for further development by the USAAC.
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.