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Britain's Vickers Wellesley bomber1,2
| Vickers Wellesley bomber: |
Vickers Wellesley bomber: |
Vickers Wellesley Mk I bomber: |
Vickers Wellesley Mk I bomber: |
Vickers Wellesley bomber:![]() |
Vickers Wellesley bomber:![]() |
Design
The Vickers Wellesley was the first Royal Air Force (RAF) aircraft designed to used Barnes Wallis' geodetic construction method.1,2 The Air Ministry put forth a specification for a biplane torpedo bomber.1 Vickers submitted a design for a biplane and monoplane aircraft.1 The monoplane was superior and was selected.1
Wings
The wings had a long span and high aspect ratio, which allowed for cruising efficiency.1 Panniers under the wings housed the bombs.1
Prototype
The Wellesley prototype first flew on June 19, 1935.1,2 An order for 96 was placed in September 1935.1,2
Production
The first Wellesley Mk I flew on January 30, 1937.1 The Wellesley entered service in April 1937.1 The last Wellesley was delivered in May 1938.1
- Prototype: 11
- Wellesley Mk I: 1761,2
- Total: 1771
Variants
- Prototype:
- Wellesley Mk I:
- Wellesley Mk II: Some Mk Is were fitted with a continuous canopy glazing and were referred to as the Mk II.1
Usage
Ten RAF squadrons were equipped with the Wellesley.1
Record Breaking
In November 1938 three Wellesleys took off from Ismailia, Egypt and flew to Darwin, Australia non-stop.1,2 They had extra fuel tanks installed.1 Two of them made the journey of 7,162 miles / 11,526 km in a little over 48 hours.1,2
Start of World War II
At the start of the war there were about 100 Wellesleys based in the Middle East and Africa.1 They such much action against the Italian's in East Africa, Italian Somaliland, and the Western Desert.1
Later these aircraft were used for shipping reconnaissance until the middle of 1943.1
| Vickers Wellesley Mk I1,2 | |
|---|---|
| Type | General purpose bomber1, Bomber2 |
| Crew | 21,2 |
| Engine (Type) | Bristol Pegasus XX1,2 |
| Cylinders | Radial 91,2 |
| Cooling | |
| HP | 9251,2 |
| Propeller blades | 31 |
| Dimensions | |
| Span | 74' 7"1,2 22.73 m1 |
| Length | 39' 3"1,2 11.96 m1 |
| Height | 12' 4"1,2 3.76 m1 |
| Wing area | |
| Weight | |
| Empty | 6,369 lb1 2,889 kg1 |
| Loaded | 11,100 lb1,2 5,035 kg1 |
| Performance | |
| Speed at sea level | 178 mph1 286 kph1 |
| Speed @ 19,680' | 228 mph2 |
| Speed @ 19,700' / 6,005 m |
228 mph1 370 kph1 |
| Cruising speed | 160 mph1 257 kph1 |
| Climb | 1,200'/minute1 365 m/minute1 |
| Service ceiling | 26,100'1, 33,000'2 7,955 m1 |
| Range | 1,110 miles2, 1,335 miles1 2,148 km1 |
| Armament | 2: MGs2 |
| Nose | 1: 0.303" MG1 |
| Rear cockpit | 1: 0.303" MG1 |
| Bombs | 2,000 lb2 |
| Bombs - under wing pods | 2,000 lb1 907 kg1 |
Sources:
- Aircraft of WWII, Stewart Wilson, 1998
- World War II Airplanes Volume 1, Enzo Angelucci, Paolo Matricardi, 1976


