General Electric tunnel test with F-104A 60763 The F-104 was designed to use the General Electric J79 turbojet engine, fed by side-mounted intakes with fixed inlet cones optimized for supersonic speeds. Unlike some supersonic aircraft, the F-104 did not have variable-geometry inlets. Its thrust-to-drag ratio was excellent, allowing a maximum speed well in excess of Mach 2. The initial assembly of 56-763 was finished on July 18, 1957 and accepted by the US Air Force on August 26, 1957. August 29, it was delivered directly to the General Electric test-site at Edwards Air Force Base. With this testgroup it was used for testing the J79-7 engine until March 1958 when it was given to the AFFTC at Edwards. In March 1962 it returned back with General Electric for accelerated service tests on the J79-3B engine version. The aircraft got dayglow areas painted and also nickname "Queenie II" replacing the former General Electric Starfighter 56-742. copyright © NACA archive