Kazakh VS Decree 'On renaming town of Zarya to Leninsk at site 10 at Tyuratam' was issued.

Last test of the original R-7 8K71 test series. Suborbital launch test.

NASA announced the award of a $1.356 million contract to the Blaw-Knox Company for design and construction of three parabolic antennas, each 26 meters (85 feet) in diameter, for the Manned Space Flight Network stations at Goldstone, Calif.; Canberra, Australia; and near Madrid, Spain.

First first mission of Block II Saturn with two live stages. SA-5, a vehicle development flight, was launched from Cape Kennedy Complex 37B at 11:25:01.41, e.s.t. This was the first flight of the Saturn I Block II configuration (i.e., lengthened fuel tanks in the S-1 and stabilizing tail fins), as well as the first flight of a live (powered) S-IV upper stage. The S-1, powered by eight H-1 engines, reached a full thrust of over 680,400 kilograms (1.5 million pounds) the first time in flight. The S-IV's 41,000 kilogram (90,000-pound-thrust cluster of six liquid-hydrogen RL-10 engines performed as expected. The Block II SA-5 was also the first flight test of the Saturn I guidance system.

ASPO concurred with the requirement to provide an emergency defecation capability aboard the LEM as established by MSC's Center Medical Programs Office. The addition of a Gemini-type defecation glove appeared to present a satisfactory solution. Crew Systems Division was directed to proceed with their recommendation and add the Gemini gloves to the LEM crew provisions.

Apollo boilerplate 28 underwent its second water impact test. Despite its strengthened aft structure, in this and a subsequent drop on February 9 the vehicle again suffered damage to the aft heatshield and bulkhead, though far less severe than that experienced in its initial test. The impact problem, it was obvious, was not yet solved.

The first manned test of the airlock fails before an audience of 60 government and industry leaders. A VVS pilot in a spacesuit was to demonstrate the entire sequence involved in exiting into space. (release of the forward ring, inflation of the airlock, opening of the hatch between the spacecraft and airlock, closing the hatch, evacuation of the air from the airlock, opening of the outer hatch of the airlock, then the sequence in reverse). Two attempts are made at 15 km equivalent altitude, but the hatch from the spacecraft to the airlock cannot be opened due to defects in its construction in the first try. This is fixed, but on the second try the Vega system that monitors the cosmonaut's condition fails.

Nomenclature for the OWS included in the AAP presented in the FY 1969 budget was confirmed by NASA. The ground-outfitted OWS to be launched with Saturn V would be designated the 'Saturn V Workshop.' (This had sometimes been called the 'dry Workshop.') The OWS that would be launched by a Saturn IB would be referred to as the 'Saturn I Workshop.' (Colloquially it had been referred to as the 'wet workshop.') Terminology 'Uprated Saturn I' would not be used officially. This launch vehicle would be referred to as the 'Saturn IB.'

Review of spacesuit development at Zvezda Factory with Gay Severin. The specifications for the moon suit are 10 hours life, 80 kg mass, able to handle a heat load of 500 kcal/hour. But this load is insufficient for heavy work. By comparison, the suits used by Leonov and Khrunov could only handle 200-250 kcal/hour. 14 suits have been completed for tests. In the afternoon Soyuz descent systems are reviewed at Aleksander Lobanov's institute. The descent system parachutes are rated for a 10 tonne payload, but 40 tonnes of force are required to pull the parachute out of the compartment in the capsule. Individual parachutes could be provided for the crew, weight 6 kg each. This would evidently be considered as the back-up on L1 and LOK flights where the capsule had a side hatch and no reserve parachute.

The audit reveals that the institute should receive an 850,000 rouble budget increase, and construct new training facilities.

The space vehicle for the Apollo 14 mission was determined ready for launch on January 31. The Flight Readiness Review had been held at KSC on December 17, 1970; all required action and open work had been completed; and the Pre-Liftoff Readiness Review had been favorably completed January 29.

Three DOS-7K crews are to fly on two Tu-104's to Baikonur on 30 January. The Tu-104's are fitted with the Svinets equipment, which the cosmonauts will use to capture spectral data on two rocket launches. This training will prepare them for use of the Svinets equipment aboard the DOS station. Lots of bigwigs from the VVS plan to tag along as well.

Area survey photo reconnaissance satellite; returned film capsule.

Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Launch vehicle put payload into geosynchronous transfer orbit Positioned in geosynchronous orbit over the Atlantic Ocean at 29.5 deg W in 1976-79; over the Atlantic Ocean 27.5 deg W in 1979-1980; over the Atlantic Ocean 21.5 deg W in 1980-1983; over the Indian Ocean 57 deg E in 1983-1984; over the Atlantic Ocean 2-4 deg W in 1984-1985 As of 3 September 2001 located at 151.88 deg E drifting at 2.088 deg W per day. As of 2007 Mar 10 located at 130.98W drifting at 2.123W degrees per day.

Radar calibration; replaced Cosmos 1186. Released 25 Romb radar calibration subsatellites.

First launch of a prototype DFH-2 communications satellite. Payload stranded in low earth orbit, but all subsystems including the communications payload were completely checked and tested.

Civilian naval navigation satellite.

Prototype satellite for the planned Koskon (Space Conversion) Global Space Communication System. It was planned that the Koskon constellation would consist of a constellation of 32 to 45 satellites in 1997-2001. Also carried amateur radio transponders and performed geological research. Routine communications, collection and relaying of information in the interests of the Ministry of Geology of the USSR and other branches of the country's national economy, and the development of communications between amateur radio-operators.

Glonass navigational satellite. Testing of components and apparatus of the Glonass global space navigation system being set up to determine the position of civil aircraft and vessels of the merchant marine and fishing fleet.

Glonass navigational satellite. Testing of components and apparatus of the Glonass global space navigation system being set up to determine the position of civil aircraft and vessels of the merchant marine and fishing fleet.

Glonass navigational satellite. Testing of components and apparatus of the Glonass global space navigation system being set up to determine the position of civil aircraft and vessels of the merchant marine and fishing fleet.

UHF Follow-On #4; US Navy communications . Stationed at 177.0 deg W. Launch vehicle put payload into subsynchronous earth orbit with MRS trajectory option. Positioned in geosynchronous orbit at 177 deg W in 1995-1999.

Soyuz TM-27 carried the Mir EO-25 crew and French astronaut Leopold Eyharts. NASA and the Russian Space Agency had hoped Soyuz TM-27 could dock with Mir while Endeavour was still there, resulting in an on-board crew of 13, a record which would have stood for years or decades. But the French vetoed this, saying the commotion and time wasted would ruin Eyharts Pegase experimental programme. Soyuz TM-27 docked at the Kvant module port at 17:54 GMT on January 31, 1998, less than five hours before Endeavour landed in Florida.

Solovyov handed over command of Mir to EO-25 commander Musabayev, and the Mir EO-24 crew and Eyharts undocked from the forward port of Mir at 05:52 GMT on February 19 aboard the Soyuz TM-26 for their return home. On February 20, the EO-25 crew and Andy Thomas of the NASA-7 mission boarded Soyuz TM-27 and undocked from the Kvant port at 08:48 GMT. They redocked with the forward port on Mir at 09:32 GMT. This freed up the Kvant port for a test redocking of the Progress M-37 cargo ship, parked in a following orbit with Mir during the crew transfer.

Classified satellite for the National Reconnaissance Office. It was likely that it was a technology test satellite combining equipment for several future projects, including a prototype COBRA BRASS infrared early warning satellite sensor. The project seemed to have been several years behind schedule (based on the launch vehicle serial number.

Launch delayed from June 11 and August 16, 2001; March 6, April 29, August 11 and November 7, 2002.

On-orbit servicing technology demonstrator. XSS-10, a 28 kilogram microsatellite, was launched as a secondary payload aboard the Delta 2 launch vehicle carrying a Global Positioning Satellite (GPS) satellite. The mission demonstrated the complex interactions of line-of-sight guidance with basic inertial maneuvering. The micro-satellite was attached to the Delta 2 second stage. Once the second stage separated from the GPS satellite, the microsatellite waited for a sunlit Air Force Space Control Network pass before ejecting from the second stage. Once ejected, the microsatellite commenced an autonomous inspection sequence around the second stage, and live video was transmitted to ground stations. The entire mission lasted only 24 hours. Launch delayed from June 11 and August 16, 2001; March 6, April 29, August 11 and November 7, 2002.

ISS resupply, to dock at the Zvezda module of the station 13:15 GMT on 31 January. Launch delayed from November 20, 2003. Payload delivered amounted to 2345 kg and included a new flex hose for the Destiny module's leaky window, replacement parts for the Russian Elektron oxygen-generating unit, a spare Elektron, new Russian Solid Fuel Oxygen Generator candles, batteries for the Zarya and Zvezda modules, gas analyser equipment, updated fire suppression and detection equipment, a new Russian Orlan spacesuit, film, cameras, data cassettes and the Matreshka experiment package for installation on Zvezda's exterior during a spacewalk.

A few days prior to its departure from the ISS, ground controllers fired the Progress M1-11's engines for 11 minutes, boosting the Station's altitude by 3.7 km and adjusting its inclination by one one-hundredth of a degree. Progress M1-11 undocked from the Station at 11:19 GMT on 24 May 2005, clearing the way for the arrival of Progress M-49. It was thereafter commanded to a destructive re-entry over the Pacific Ocean.