Saunders-Roe SR.53

The Saunders-Roe SR.53 was a British prototype interceptor aircraft of mixed jet and rocket propulsion developed for the Royal Air Force (RAF) by Saunders-Roe in the early 1950s. As envisaged, the SR.53 would have been used as an interceptor aircraft, using its rocket propulsion to rapidly climb and approach incoming hostile bombers at high speeds; following its attack run, the aircraft would then return to its base using jet propulsion. Although the SR.53 proved to have promising performance during test flights, the requirement for such an aircraft had been overtaken by rapid advances in surface-to-air missile technology, leading to reconsideration of the aircraft's purpose. In July 1960, the development programme was formally cancelled, by which time a total of 56 test flights had been performed. A pair of prototype SR.53 aircraft had been completed and used during flight tests. The second prototype was destroyed during one such test flight in June 1958. The first prototype has been preserved to this day. It rests on public display at the Royal Air Force Museum Cosford.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Saunders-Roe
- First flight
- 1957-05-16
Specifications
- Max speed
- 2.2 kt
- Service ceiling
- 67,000 ft
- Rate of climb
- 52,000 ft/min
- Max takeoff weight
- 18,400 lb
- Empty weight
- 7,400 lb
- Powerplant
- Armstrong Siddeley ASV.8 Viper 8 turbojet and de Havilland Spectre liquid-fuelled rocket
- Engines
- 2
- Seats
- 1
- Length
- 45 ft
- Wingspan
- 25.1 ft
- Height
- 10.8 ft
- Number built
- 2
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.