Armstrong Siddeley Screamer
The Armstrong Siddeley Screamer was a rocket engine intended to power the Avro 720 manned interceptor aircraft (Avro's competitor to the Saunders-Roe SR.53 for a rocket-powered interceptor). Thrust was variable, up to a maximum of 36 kN (8,000 lbf).
|Country of origin||Britain|
|Date||March 1954 (first static test)|
|Propellant||liquid oxygen (LOX) / methanol|
Work on the Screamer started in 1946, with the first static test at Armstrong Siddeley's rocket plant at Ansty in March 1954. The programme was cancelled, as was the Avro 720, before flight testing.
In 1951, a Gloster Meteor F.8 was experimentally fitted with a Screamer mounted below the fuselage.
- "Armstrong Siddeley Screamer". Flight (PDF): 160–164. 27 July 1956.
- Allen, S., RAeS (7 December 1951). "Rockets for Aircraft Propulsion". The Aeroplane.
- Allen, S., RAeS (19 October 1956). "ROCKET-MOTOR DESIGN:A Paper by the Chief Engineer of Armstrong Siddeley Motors (Rocket Division)". Flight (PDF): 637–638. Retrieved 27 November 2014.
- "Scorpion and Screamer" (PDF). Flight: 76. 13 July 1956.
- C.N. Hill (2001). A Vertical Empire: The History of the UK Rocket and Space Programme, 1950-1971. Imperial College Press. p. 28. ISBN 1-86094-268-7.
- Keith Meggs. "A Man and his Machines".
- "Cancelled projects: the list up-dated" (PDF). Flight: 262. 17 August 1967.
- "Sectional drawing of the Screamer" (image). Flight International. External link in