Flight of Goddard liquid fuel rocket with new gasoline shutoff valve. Dimensions similar to October 13; altitude 1330 ft; landed 930 ft from tower; in air 8.6 sec. References: 482 .
Composition research. Launched at 0630 local time. Reached 80.2 km.
A special Committee on Life Sciences was established at Langley to determine qualifications and attributes required of personnel to be selected for America's first manned space flight and to give advice on other human aspects of the manned satellite program. References: 483 .
Space Task Group (STG), assisted by George M. Low, NASA Assistant Director for Space Flight Operations, and Warren J. North of Low's office, prepared a project summary presenting a program of manned spaceflight for 1963-1965. This was the final version of the Project Development Plan, work on which had been initiated August 14. Additional Details: Program of manned spaceflight for 1963-1965..
Secretary of Defense McNamara announced that progress of the Administration's accelerated defense buildup made unnecessary the use of additional defense funds appropriate by the Congress above the amount requested by the administration. The Congress had voted $514.5 million for additional long-range bombers; $180 million additional for the B-70; and $85.8 million additional for Dyna-Soar. References: 18 .
Largest known rocket launch to date, the Saturn I 1st stage booster, successful on first test flight from Atlantic Missile Range. With its eight clustered engines developing almost 1.3 million pounds of thrust at launch, the Saturn (SA-1) hurled waterfilled dummy upper stages to an altitude of 84.8 miles and 214.7 miles down range. In a postlaunch statement, Administrator Webb said: "The flight today was a splendid demonstration of the strength of our national space program and an important milestone in the buildup of our national capacity to launch heavy payloads necessary to carry out the program projected by President Kennedy on May 25.". References: 5 , 26 , 27 .
First attempted launch of Cosmos 63S1 small launch vehicle.
NASA announced the appointment of Major General Samuel C. Phillips as Director of the Apollo Program. Phillips thus assumed part of the duties of George E. Mueller, Associate Administrator of Manned Space Flight, who had been serving as Apollo Director as well. Phillips had been Deputy Director since January 15. References: 16 .
Suborbital test of subscale model of X-20 Dynasoar. Aero-environmental test vehicle (AEV) to test aerodynamic properties of flexing outer skin with corrugated columbium panel. Reached 4,000 m/s at 50.6 km altitude before being released from launch vehicle. Telemetry received for 900 seconds until spaceplane had reached Mach 2 1200 km downrange. It then became unstable and crashed into the Atlantic. Recovery was not planned. References: 5 .
DF-2 launched with 20 kt warhead from Shaunchengtzu 800 km to Lop Nor, where warhead successfully explodes. References: 87 .
Docked with Cosmos 188; First automated docking. Recovered October 31, 1967 08:20 GMT. Achieved automatic rendezvous on second attempt. Capture achieved but hard docking and electric connections unsuccessful due to misallignment of spacecraft. Star tracker failed and had to make a high-G ballistic re-entry. Additional Details: Cosmos 186. References: 1 , 2 , 6 .
Stationed at 24.5 deg E. At the time, the Intelsat 6 series were the largest commercial spacecraft ever built. The series were also the first commercial satellites to employ Satellite Switched/Time Division Multiple Access (SS/TDMA) techniques. Spacecraft: Based on Hughes 393 bus. Spin stabilised with despun antenna. Hydrazine propulsion system. Passive thermal control. Telescoping dual-cylinder structure with deployed antennas. Body mounted solar cells generate 2250 W (EOL). Solar drums are each about 6m tall. Payload: 38 (plus 12 backup) C-Band and 10 (plus 4 backup) Ku-Band transponders.120,000 telephone calls and 3 colour TV broadcasts simultaneously. SS/TDMA (Satellite-Switched Time Division Multiple Access) techniques used. References: 1 , 2 , 5 , 6 .
Reflector mirror, deployed from Progress M-15 after separation from Mir space station. References: 279 .
Unmanned resupply vessel to Mir. Docked with Mir on 29 Oct 1992 19:05:51 GMT. Undocked on 4 Feb 1993 00:44:53 GMT. After completion of the Znamya and autonomous operation experiments, destroyed in reentry on 7 Feb 1993 06:43:20 GMT. Total free-flight time 5.32 days. Total docked time 97.24 days. References: 1 , 2 , 6 , 275 .
Communications satellite; failed to reach orbit.