United States' Vultee A-35 Vengeance dive bomber
Design
As a result of the success of the Junkers Ju 87 in the Spanish Civil War Britain wanted a dive bomber for the Royal Air Force (RAF).1,2
Prototype
The Vultee prototype first flew in July 1941.1
Production
In 1940 700 Vultee V-72s were ordered by the British.1
- Vultee A-31 / Vultee Vengeance Mk I: 4001
- Vultee A-31 / Vultee Vengeance Mk IA: 2001
- Vultee V-72 / Vultee Vengeance Mk II: 3001
- Vultee A-31 / Vultee Vengeance Mk III: 1001
- Vultee A-35A: 1001
- Vultee A-35B / Vultee Vengeance Mk IV: 8311
- Total: 1,5282, 1,9311
- Manufacturer: Vultee Aircraft Inc.1,2, Northrop1
Usage
The Vultee Vengeance was used by Australia (342), Brazil (29), Britain (1,2052 / 1,220), India(~30), and the United States (3232).1
Unkind Words
In 1943 a United States Army Air Force (USAAF) General stated that the Vengeance was "a shining example of waste of material, manpower, and time.1,2
Britain
Britain started to receive deliveries of the V-72 in late 1942.1
Australia
The Royal Australian Air Force (RAAF) had five squadrons equipped with Vengeances operating in New Guinea.1 After it was discovered the Vengeance was unstable they were converted to communication and target tug aircraft.1
United States
The USAAF received 99 A-35s and 243 of the Vengeance Mk IIs that were diverted from Britain's order.1 These too eventually became target tugs.1,2
| Vultee Vengeance1 | Vultee Vengeance A-311 | Vultee Vengeance A-35A1,2 | Vultee Vengeance A-35B1 | |
|---|---|---|---|---|
| Type | Dive bomber1 | Bomber2 | ||
| Crew | 21 | 22 | ||
| Engine (Type) | Wright R-2600-19 Cyclone1 | Wright R-2600-13 Cyclone2, Wright R-2600-19 Cyclone1 | Wright R-2600-13 Cyclone1 | |
| Cylinders | Radial 141 | Radial 141,2 | Radial 141 | |
| Cooling | Air2 | |||
| HP | 1,6001 | 1,6001, 1,7002 | 1,7001 | |
| Propeller blades | 31 | 31 | 31 | |
| Dimensions | ||||
| Span | 48'1 14.63 m1 |
48'2 | ||
| Length | 39' 9"1 12.11 m1 |
39' 9"2 | ||
| Height | 15' 4"1 4.67 m1 |
15' 4"2 | ||
| Wing area | ||||
| Weight | ||||
| Empty | 10,300 lb1 4,672 kg1 |
|||
| Loaded | 14,300 lb1 6,486 kg1 |
16,400 lb2 | 16,400 lb1 7,439 kg1 |
|
| Performance | ||||
| Speed @ 13,500' / 4,115 m |
279 mph2 | 279 mph1 449 kph1 |
||
| Cruising speed | 230 mph1 370 kph1 |
|||
| Climb | 1,200'/minute1 366 m/minute1 |
|||
| Climb to 15,000' / 4,570 m |
11.3 minutes1 | |||
| Service ceiling | 22,300'2 | 22,300'1 6,800 m1 |
||
| Range | 2,300 miles2 | 600 miels1 965 kph1 |
||
| Maximum range | 2,300 miles1 3,700 km1 |
|||
| Armament | 5: MG2 | |||
| Wings | 4: 0.303" MG1 | 4: 0.5" MG1 | 6: 0.5" MG1 | |
| Rear cockpit | 2: 0.303" MG1 | 1: 0.5" MG1 | ||
| Bombs | 2,000 lb1 907 kg1 |
2,000 lb2 |
Sources:
- Aircraft of WWII, Stewart Wilson, 1998
- World War II Airplanes Volume 2, Enzo Angelucci, Paolo Matricardi, 1976

