Concord supersonic airliner, jointly produced by Sud Aviation and British Aircraft Corp, will be powered by Bristol Siddeley Olympus engines; these will be able to use existing aviation kerosene fuels for flight at speed of Mach 2.2; it probably may not be necessary to introduce thermal stability requirement into existing fuel specifications; since existing synthetic turbine engine lubricants are not quite good enough, some improvement is required, particularly in connection with thermal stability at high operating temperatures; description of 3 test rigs to evaluate gas turbine engine lubricants.
Fuel and engine lubricant requirements for concord
SAE -- Paper
SAE Meeting ; 1964
1964
8 pages
Conference paper
English
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