The General Assembly of the United Nations unanimously approved Resolution 1472 (XIV), establishing the Committee on the Peaceful Uses of Outer Space to replace the Ad Hoc Committee. There were no meetings of the Committee until November 27, 1961, because of failure to agree on the composition of the Committee.
The first Oscar Phase I amateur satellite was launched piggyback with Discover 36. A group of enthusiasts in California formed Project OSCAR and persuaded the United States Air Force to replace ballast on the Agena upper stage with the 4.5 kg OSCAR I package. The satellite was box shaped with a single monopole antenna and battery powered. The 140 mW transmitter onboard discharged its batteries after three weeks. 570 Amateurs in 28 countries reported receiving its simple 'HI-HI' morse code signals on the VHF 2 meter band (144.983 MHz) until January 1, 1962. The speed of the HI-HI message was controlled by a temperature sensor inside the spacecraft. OSCAR I re-entered the atmosphere January 31, 1962 after 312 revolutions. Additional Details: here....
Owen E. Maynard, Head of MSC's Spacecraft Integration Branch, reported on his preliminary investigation of the feasibility of modifying Apollo spacecraft systems to achieve a 100-day Earth- orbital capability. His investigation examined four basic areas: (1) mission, propulsion, and flight time; (2) rendezvous, reentry, and landing; (3) human factors; and (4) spacecraft command and communications. Although modifications to some systems might be extensive- and would involve a considerable weight increase for the vehicle-such a mission using Apollo hardware was indeed feasible.
Thiokol Chemical Corporation's Wasatch Division fired its first 156-inch, one-segment, solid rocket motor (156-1-T) with gimballed nozzle thrust vector control. The motor produced approximately 1.3 million pounds of thrust for two minutes. This was the third test firing of a 156-inch solid rocket motor in Space Systems Division's Large Solid Rocket Motor Program (Program 623A).
The Titan 2 engines shut down a moment after ignition. The fault that caused the Titan to shut down saved the astronaut's lives; the quick thinking of the astronauts in not pulling the abort handles saved the mission. The scheduled launch of Gemini VI-A was aborted when the Master Operations Control Set automatically shut down the Gemini launch vehicle a second after engine ignition because an electrical umbilical connector separated prematurely. The launch was canceled at 9:54 a.m., e.s.t. Emergency procedures delayed raising the erector until 11:28, so the crew was not removed until 11:33 a.m. Launch was rescheduled for December 15. Routine analysis of the engine data, begun immediately after shutdown, revealed decaying thrust in one first stage engine subassembly before shutdown had been commanded. The problem was diagnosed as a restriction in the gas generator circuit of the subassembly, which would have caused shutdown about 1 second later than it actually occurred as a result of the umbilical disconnect. Source of the restriction proved to be a protective dust cap inadvertently left in place in the gas generator oxidizer injector inlet port. The anomalies were corrected and recycling, based on long-prepared contingency plans, proceeded without incident through launch on December 15.
Since Soyuz 11 and his subsequent 'retirement', the Soviet Union has launched two space stations that failed in orbit, and made only one two-day Soyuz flight. Meanwhile the Americans had run successfully their entire Skylab program. The fourth N1 exploded on 23 November 1972. Ustinov has thrown away tens of billions of roubles on that useless project. Soyuz 13 landed yesterday - the first Soviet manned spaceflight not under Kamanin's command. Khrushchev made many mistakes, but Brezhnev continues to make even more. Kamanin feels his country is however not fit for democracy, that it needs discipline - otherwise there will be anarchy.
First successful North Korean satellite launch. Amateur observations showed the satellite to be tumbling, and no signals were picked up at the announced 470 MHZ frequency - it was assumed the spacecraft never functioned or failed shortly after orbital insertion.