The NII-1 NKAP research institute was formed with Mstislav Vsevolodovich Keldysh as its head to investigate and develop the German Saenger-Bredt design. It was clear from the preliminary study that an immense amount of work needed to be done before a draft project of a feasible design could be prepared - it would take until the mid-1950's.

Launched at 0823 hours EST from AMR. The flight was successful. Actual range was 138.969 nm; .137 nm over and 122 meters left of the intended impact point, a radial miss distance of 260 meters. The primary test objectives were to test the accuracy of the complete guidance system and to test Jupiter control components. Missed aimpoint by 255 m.

President Dwight D. Eisenhower recommended to Congress the formation of an Advanced Research Projects Agency (ARPA) in a Defense Department reorganization proposal. The new agency would provide unified Defense Department direction and management of certain advanced research and development projects.

A joint briefing on the Apollo and Saturn programs was held at Marshall Space Flight Center MSFC, attended by representatives of STG and MSFC. Maxime A. Faget of STG and MSFC Director Wernher von Braun agreed that a joint STG-MSFC program would be developed to accomplish a manned lunar landing. Areas of responsibility were: MSFC launch vehicle and landing on the moon; STG - lunar orbit, landing, and return to earth.

Astronaut John Glenn was selected as the pilot for the first Mercury manned orbital flight, with Scott Carpenter as backup pilot. Immediately, training was started to ready these two astronauts for the mission. The five remaining astronauts concentrated their efforts on various engineering and operational groups of the Manned Spacecraft Center in preparation for the mission.

Atlas D (53D) was the first missile to be launched by SAC from Vandenberg in the operation test (Category III) launch program. Mercury-Atlas 5 (MA-5), the second and final orbital qualification of the spacecraft prior to manned flight was launched from Cape Canaveral with Enos, a 37.5 pound chimpanzee, aboard. Scheduled for three orbits, the spacecraft was returned to earth after two orbits due to the failure of a roll reaction jet and to the overheating of an inverter in the electrical system. Both of these difficulties could have been corrected had an astronaut been aboard. The spacecraft was recovered 255 miles southeast of Bermuda by the USS Stormes. During the flight, the chimpanzee performed psychomotor duties and upon recovery was found to be in excellent physical condition. The flight was termed highly successful and the Mercury spacecraft well qualified to support manned orbital flight.

Academic examinations were completed of the female cosmonaut corps. Kuznetsova had missed to much training and was excluded from even taking the test. Of the four women remaining, only Tereshkova did not receive the highest marks. This was attributed to her being too nervous and excited during the examination. All were given the rank of Junior Lieutenant in the VVS Soviet Air Force.

Kamanin considered Tereshkova as the leading candidate for the first flight, with Solovyova as her back-up. In personality they were equivalent to Gagarin/Nikolayev - indeed, Tereshkova was considered 'Gagarin in a skirt'. Ponomaryova and Yerkina were equal candidates for the second female Vostok flight. The group would go to a resort in the Urals from 30 November to 10 January. The final decision as to which one would fly would only be made 3 or 4 days before the flight.

Ground was broken at Edwards AFB, California for construction of the largest and most heavily instrumented solid-rocket motor test facility. It was designed to test the five-segment, 120-inch solid-propellant motors for the Titan III program but could handle engines up to and including 156 inches in diameter.

Ionospheric research; data correlated with Explorer 31. The double-launch project, known as ISIS-X was the first in a new co-operative NASA-Canadian Defense Research Board program for International Satellites for Ionospheric Studies. Alouette was in orbit with an apogee just over a kilometre lower than Explorer 31's and with a perigee of just more than a kilometre higher. The orbits were some 3000 km at apogee and 500 km at perigee.

Ionospheric research; data correlated with Alouette 2. The Explorer 31, Direct Measurement Explorer, was launched with a Canadian Alouette II on November 28, 1965, on a Thor-Agena rocket from Vandenberg Air Force Base, California. The double-launch project, known as ISIS-X was the first in a new co-operative NASA-Canadian Defense Research Board program for International Satellites for Ionospheric Studies. Explorer 31 was in orbit with an apogee just over a kilometre more than Alouette's and with a perigee of just more than a kilometre lower. The orbits were some 3000 km at apogee and 500 km at perigee. Eight ionospheric measurement experiments sampled the environment both forward and after the satellite's path.

Kamanin writes a letter to the Central Committee on the need for the 7K-VI spacecraft for military research. He also complains about his problems in obtaining adequate spacecraft simulators. Later he meets with Grigoriy Nikolayevich Postukov, sculptor of cosmonaut statutes.

Unmanned military Soyuz 7K-S test flight. Recovered December 17, 1976 10:31 GMT. Transmitted only on 20.008 MHz and 166 MHz frequencies, at none of the other usual Soyuz wavelengths.
Maneuver Summary:
196 km X 290 km orbit to 187 km X 335 km orbit. Delta V: 15 m/s
187 km X 335 km orbit to 259 km X 335 km orbit. Delta V: 21 m/s
259 km X 335 km orbit to 260 km X 345 km orbit. Delta V: 2 m/s
260 km X 345 km orbit to 265 km X 368 km orbit. Delta V: 7 m/s
265 km X 368 km orbit to 267 km X 391 km orbit. Delta V: 6 m/s
267 km X 391 km orbit to 300 km X 310 km orbit. Delta V: 32 m/s
Total Delta V: 83 m/s

Reserve DSP ballistic missile launch detection satellite fitted with Block 14 sensors, remained in service for only five years.. Observed Scud launches during Gulf War. Positioned in geosynchronous orbit at 35 deg W in 1988-1989; 10 deg E in 1989-1992; 35 deg W in 1992-1993; 105 deg E in 1993; 165 deg W in 1999.

34 Ku-band transponders for TV. Stationed at 37.48 deg W. Launch vehicle put payload into supersynchronous earth orbit with IFR trajectory option. Positioned in geosynchronous orbit at 37 deg W in 1994-1999 As of 5 September 2001 located at 37.54 deg W drifting at 0.010 deg W per day. As of 2007 Mar 11 located at 37.60W drifting at 0.015W degrees per day.

The first test launch of a DFH-3 by a CZ-3A launch vehicle was successful in attaining the proper transfer orbit, but during the subsequent manoeuvres to achieve geostationary orbit, the DFH-3 failed due to a malfunction of the satellite on-board propulsion system. The satellite was positioned at 132 deg E prior to the failure. As of 4 September 2001 located at 113.80 deg E drifting at 2.499 deg E per day. As of 2007 Mar 2 located at 90.02E drifting at 2.513E degrees per day.

The EO-10 crew entered Soyuz TMA-5, undocked it from the Pirs module of the International Space Station at 09:32 GMT and redocked it at the nearby Zarya module at 09:53 GMT. This cleared the Pirs docking port for the expected arrival of a Progress unmanned logistics spacecraft.