|Mission duration||2 days, 12 minutes, 11 seconds|
|Spacecraft type||Soyuz 7K-T/A9|
|Launch mass||6,760 kilograms (14,900 lb)|
|Callsign||Дунай (Dunay - "Danube")|
|Start of mission|
|Launch date||August 26, 1974, 19:58:05UTC|
|Launch site||Baikonur 1/5|
|End of mission|
|Landing date||Did not recognize date. Try slightly modifying the date in the first parameter. UTC|
|Landing site||48 kilometres (30 mi) SW of Tselinograd|
|Perigee||173 kilometres (107 mi)|
|Apogee||236 kilometres (147 mi)|
Launched 26 August 1974, the Soyuz spacecraft arrived at the station, but cosmonauts Lev Dyomin and Gennadi Sarafanov were unable to dock because the electronics in the Igla docking system malfunctioned. Without sufficient fuel for prolonged attempts at manual docking, the mission had to be abandoned. The cosmonauts powered down all nonessential systems in the Soyuz and waited until the next day for reentry. The crew landed 28 August. Analysis of the launch window was cited by observers for concluding a flight of 19 to 29 days had been planned.
In the event of the failure, official TASS statements merely claimed that the mission was intended to practice docking maneuvers with the Salyut 3 station. They also said that a new automatic docking system was tested which would be used on future Progress transport craft.
The failed mission exposed a number of serious design flaws in the Soyuz 7K-T spacecraft, namely its lack of reserve propellant and electrical power for repeated docking attempts. In addition, the Igla docking system was found to be in major need of improvement. Since it was impossible to carry out these changes before Salyut 3 finished its operating lifespan, they had to wait for future space stations. The backup spacecraft for the Soyuz 15 mission was placed in storage and later flown as Soyuz 20 despite being past its intended shelf life.
- Backup crew 1.1
- Reserve crew 1.2
- Mission parameters 2
- References 3
|Flight Engineer||Vitaly Zholobov|
|Flight Engineer||Valery Rozhdestvensky|
- Mass: 6,760 kg (14,900 lb)
- Perigee: 173 km (107 mi)
- Apogee: 236 km (147 mi)
- Inclination: 51.6°
- Period: 88.5 min
- "Baikonur LC1". Encyclopedia Astronautica. Retrieved 2009-03-04.
- Clark, Phillip (1988). The Soviet Manned Space Program. New York: Orion Books, a division of Crown Publishers, Inc.
- Newkirk, Dennis (1990). Almanac of Soviet Manned Space Flight. Houston, Texas: Gulf Publishing Company.