United States (cancelled)
(OPERATORS list includes past, present, and future operators when applicable)
Width/Span
52.5 ft
(16.00 m)
Empty Wgt
13,404 lb
(6,080 kg)
MTOW
24,185 lb
(10,970 kg)
Wgt Diff
+10,781 lb
(+4,890 kg)
(Showcased structural values pertain to the base Vultee XA-41 production variant)
Installed:
1 x Pratt & Whitney R-4360 28-cylinder radial piston engine developing 3,000 horsepower.
Max Speed
364 mph
(585 kph | 316 kts)
Ceiling
29,199 ft
(8,900 m | 6 mi)
Rate-of-Climb
2,730 ft/min
(832 m/min)
♦ 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 Vultee XA-41 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:
4 x 0.50 caliber M2 Browning heavy machine guns in wings.
4 x 37mm Autocannons in wings
OPTIONAL:
Up to 6,500lbs of total stores, internally and externally. Approximately 2,000lbs internally and 1,600lbs held under the wings. Ordnance support included rockets, torpedoes and conventional drop bombs.
(Not all ordnance types may be represented in the showcase above)
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.