Secretary of Defence Wilson rules that Army could not develop missiles over 200 mile range. Jupiter assigned to AF. References: 86 .
Fired from AMR at 2110 hours EST. Main stage, lift-off, and powered flight were normal. The missile passed through the critical dynamic pressure period and followed the prescribed trajectory until 202 seconds of flight when the engine thrust was terminated. From an analysis covering the period before thrust termination, mechanical failure of the turbo-pump stopped the flow of propellants to the combustion chamber causing a complete loss of thrust. Telemetry signals ceased at 232 seconds. The missile was at an altitude of 65,000 feet when an explosion was observed from the Test Centre above the horizon. The long range mission of this flight was not accomplished; however, other primary and secondary missions were considered successful. References: 439 .
Project Mercury, U.S. manned-satellite program, was officially named by NASA. References: 17 .
An intended lunar probe launched from the Atlantic Missile Range by an Atlas-Able booster disintegrated about 45 seconds later when the protective sheath covering the payload detached prematurely. The probe was sponsored by NASA, developed by the Jet Propulsion Laboratory, and launched by the Air Force Ballistic Missile Division. References: 5 , 126 , 278 .
Christopher C. Kraft, Jr., was appointed Deputy Director of MSC. Kraft, Director of Flight Operations at MSC since November 1963, succeeded George S. Trimble, Jr., who had resigned September 30. References: 16 .
Provision of uninterrupted round the clock telephone and telegraph radiocommunication in the USSR and simultaneous transmission of colour and black-and-white USSR central television programmes to stations in the Orbita network. References: 1 , 2 , 5 , 6 , 67 , 274 .
Stationed at 95 deg E. Relaying of telephone and telegraph information. Second launch in Altair/SR system for communication with Mir space station and other orbital spacecraft. In late July 1988 Cosmos 1897 was moved from its station at 95 degrees East to 12 degrees East to support the Buran shuttle test flight of November 14, 1988. During February 1987 the satellite was moved back to its original position at 95 degrees East. The satellite drifted to 90 degrees East by March 1991. By late April it was maneuvered it back to 95 degrees East, but by the end of 1991 it had drifted to 77 degrees East and was considered inoperative. References: 1 , 2 , 5 , 6 , 67 , 274 .
Mir Expedition EO-04. Carried Alexander Volkov, Sergei Krikalev, Jean-Loup Chretien to Mir; returned Volkov, Krikalev to Earth. Initial Orbit: 194 X 235 km. Thereafter maneuvered to rendezvous orbit 256 X 291 km before docking with Mir in 337 X 369 km at 17:16 GMT 28 November. References: 1 , 2 , 6 , 51 .
Mir expansion module. Scheduled docking 2 December delayed due to failure of solar panel to extend and failure of automatic rendezvous system. Faults corrected by ground control and docked with Mir December 6, 1989 at 12:21 GMT. Transferred to lateral port December 8.
Officially: Delivery to the Mir orbital station of additional equipment and apparatus for the purpose of expanding the research and experiments conducted in the interests of science and the national economy. References: 1 , 2 , 5 , 6 , 67 , 274 .