Soyuz 13

USSR


International Flight n°: 50

Earth orbit Flight n°: 48

USSR launch Flight n°: 20


Launch, orbit & landing data:

Designation 06982 / 73103A
Launch date - time 18 Dec 1973 - 11:55 UT
Launch site Baikonur, LC1
Launch vehicle  Soyuz 11A511
OKB name - S/N° Soyuz 7K-T s/n 33A
Basic shape  Sphere-cylinder + 2 wings
Dimension (m) 7.5 long, 2.2 dia
Mass (kg) 6560
Flight Crew Klimuk, Pyotr I. (CDR)
Lebedev, Valentin V. (FE)
Call Sign Kavkaz (Caucasus M.)
Backup crew Vorobyov L., Yazdovski V.
Earth orbit on Dec 18.6:
   - Perigee / Apogee 188 x 247 km
   - Eccentricity 0.004
   - Inclination 51.57°
   - Period 88.80 min
Landing date - time 26 Dec 1973 - 08:50:35 UT
Landing location 49°N, 71°E
200km SW of Karaganda
Flight Duration (d:u:min) 7:20:55:35 (7.87 days)
Nbr orbits 127

Flight Crew

Nr. Surname Given name Job Duration Orbits
1  Klimuk  Pyotr Iliyich  Commander 7d 20h 56m  127 
2  Lebedev  Valentin Vitaliyevich  Flight engineer 7d 20h 56m  127 

Flight

Testflight of Soyuz spacecraft; biological explorations in view of later planned long-termed missions; the recovery of the capsule was problematic because of a snowstorm.

A unique flight of the 7K-T/AF modification of the Soyuz spacecraft. The main experiment carried was the "Orion 2" astrophysical observatory ("Orion 1" was carried aboard Salyut 1), the observatory obtained spectrograms of over 3000 stars, some as faint as the eleventh magnitude. The crew conducted astrophysical observations of stars in the ultraviolet range. Additional experiments included spectrozonal photography of specific areas of the earth's surface, and continued testing of space craft's on-board systems. Recovered December 26, 1973 8:50 GMT. Landed in snowstorm 200 km SW Karaganda.

After the Soyuz 11 disaster, the Soyuz underwent redesign for increased reliability. Two solo test flights of the new design were planned. The second mission would include installation of a large astrophyscial camera. Crews for the second mission, Soyuz-13, were first named in July 1973: Vorobyev/Yazdovskiy (Prime); Klimuk/Sevastyanov (Backup); Kovalenok/Ponomarev (Support). These assignments were changed a month later to: Vorobyev/Yazdovskiy(Prime); Klimuk/Ponomarev (Backup); Kovalenok/Sevastyanov (Support). They were again revised in September 1973 to Vorobyev/Yazdovskiy (Prime); Klimuk/Lebedev (Backup); Kovalenok/Ponomarev (Support). But just before launch Klimuk/Lebedev were named as the prime crew.

Maneuver Summary: 189km X 247km orbit to 186km X 255km orbit. Delta V: 2 m/s
186km X 255km orbit to 223km X 256km orbit. Delta V: 10 m/s
Total Delta V: 12 m/s.


Ref.: #1,#2, #3(SD71), #7, #8, #16, #125, #206 - update: 28.07.07 Home