Armstrong Siddeley Adder
The Armstrong Siddeley Adder was a jet engine manufactured by the British manufacturer Armstrong Siddeley from November 1948. It developed a maximum thrust of 4.67 kN.
construction and development
The Adder , a pure turbojet engine was isolated from the gas generator (core engine) of the turboprop -Triebwerks Armstrong Siddeley Mamba derived and was originally called loss engine for driving the target drone Jindivik 1 developed. It was then developed into a long-lasting variant to ultimately form the basis for the Viper .
The flight tests of the Adder ASA.1 took place on board the Avro Lancaster III with the registration SW342 in the position of the rear gunner's position. This aircraft had previously been converted by Armstrong Siddeley's flight test department in Bitteswell and used for icing tests on the Mamba.
Aircraft with Armstrong Siddeley Adder
Data (ASA.1)
General
- Type: jet engine
- Length: 1862 mm
- Diameter: 711 mm
- Weight: 250 kg
Components
- Compressor: axial, 10-stage
- Combustion chambers: 6
- Turbine: axial, 2-stage
- Fuel: kerosene
power
- Maximum thrust: 4.67 kN
- Total print ratio: 5: 1
- Push weight: 53.533 kg / kN
Individual evidence
- ^ Bill Gunston: World Encyclopedia of Aero Engines . Patrick Stephens, Cambridge 1989. ISBN 1-85260-163-9 . P. 20.
literature
- Bill Gunston: World Encyclopedia of Aero Engines . Patrick Stephens, Cambridge 1989. ISBN 1-85260-163-9
- Brian Turpin: Turbine Test Beds . Part 1 in Airplane Monthly , February 1980.
Web links
- Armstrong-Siddley - Adder on MiniJets.org. (French)
- Armstrong Siddeley Adder . Flight 1951. (English)