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Andreyev, Boris Dmitriyevich

Person · Russia

Original archive entry. The text, images and links below are kept as they were written.

Andreyev
Andreyev
Credit: www.spacefacts.de

Russian engineer cosmonaut, 1972-1983. Off flight roster for medical reasons. Civilian Engineer, Korolev OKB

More at: Andreyev.

Family
Cosmonaut
Country
Russia
Spacecraft
Salyut 6
Projects
ASTP
Bibliography
5110

Chronology

7 events

1940 October 6

  • Birth of Boris Dmitriyevich Andreyev - . Nation: Russia. Related Persons: Andreyev. Russian engineer cosmonaut, 1972-1983. Off flight roster for medical reasons. Civilian Engineer, Korolev OKB.

1972 March 22

1974 December 2

09:40 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Soyuz 16 - . Call Sign: Buran (Snowstorm ). Crew: Filipchenko, Rukavishnikov. Backup Crew: Andreyev, Dzhanibekov. Support Crew: Ivanchenkov, Romanenko. Payload: Soyuz ASTP s/n 73-EPSA. Mass: 6,800 kg (14,900 lb). Nation: Russia. Agency: MOM. Program: ASTP. Class: Manned. Type: Manned spacecraft. Flight: Soyuz 16. Spacecraft Bus: Soyuz. Spacecraft: Soyuz 7K-TM. Duration: 5.93 days. Decay Date: 1974-12-08 . USAF Sat Cat: 7561 . COSPAR: 1974-096A. Apogee: 291 km (180 mi). Perigee: 184 km (114 mi). Inclination: 51.80 deg. Period: 89.20 min.

    ASTP Manned Test Flight. Check-out of the Soyuz space craft's on-board systems which had been modernized to meet the requirements of the 1975 joint flight in accordance with the programme of the Soviet-United States experiment; conduct of scientific and technical investigations.

1975 July 15

12:20 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Soyuz 19 (ASTP) - . Call Sign: Soyuz (Union ). Crew: Kubasov, Leonov. Backup Crew: Filipchenko, Rukavishnikov. Support Crew: Andreyev, Dzhanibekov, Ivanchenkov, Romanenko. Payload: Soyuz ASTP s/n 75 (EPSA). Mass: 6,790 kg (14,960 lb). Nation: Russia. Agency: MOM. Program: ASTP. Class: Manned. Type: Manned spacecraft. Flight: Apollo (ASTP), Soyuz 19 (ASTP). Spacecraft Bus: Soyuz. Spacecraft: Soyuz 7K-TM. Duration: 5.94 days. Decay Date: 1975-07-21 . USAF Sat Cat: 8030 . COSPAR: 1975-065A. Apogee: 220 km (130 mi). Perigee: 186 km (115 mi). Inclination: 51.80 deg. Period: 88.50 min.

    Soyuz 19 initial orbital parameters were 220.8 by 185.07 kilometres, at the desired inclination of 51.80°, while the period of the first orbit was 88.6 minutes. On 17 July the two spacecraft docked. The crew members rotated between the two spacecraft and conducted various mainly ceremonial activities. Leonov was on the American side for 5 hours, 43 minutes, while Kubasov spent 4:57 in the command and docking modules.

    After being docked for nearly 44 hours, Apollo and Soyuz parted for the first time and were station-keeping at a range of 50 meters. The Apollo crew placed its craft between Soyuz and the sun so that the diameter of the service module formed a disk which blocked out the sun. After this experiment Apollo moved towards Soyuz for the second docking.

    Three hours later Apollo and Soyuz undocked for the second and final time. The spacecraft moved to a 40 m station-keeping distance so that an ultraviolet absorption experiment could be performed. With all the joint flight activities completed, the ships went on their separate ways.

1976 September 15

09:48 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Soyuz 22 - . Call Sign: Yastreb (Hawk ). Crew: Aksyonov, Bykovsky. Backup Crew: Malyshev, Strekalov. Support Crew: Andreyev, Popov. Payload: Soyuz ASTP s/n 74 modified with MF6 camera. Mass: 6,510 kg (14,350 lb). Nation: Russia. Agency: MOM. Program: ASTP. Class: Manned. Type: Manned spacecraft. Flight: Soyuz 22. Spacecraft Bus: Soyuz. Spacecraft: Soyuz 7K-MF6. Duration: 7.91 days. Decay Date: 1976-09-23 . USAF Sat Cat: 9421 . COSPAR: 1976-093A. Apogee: 296 km (183 mi). Perigee: 185 km (114 mi). Inclination: 64.80 deg. Period: 89.30 min.

    Surplus Soyuz ASTP spacecraft modified with a multi-spectral camera manufactured by Carl Zeiss-Jena in place of the universal docking apparatus. Eight days were spent photographing the earth. Tested and perfected scientific-technical methods and devices for studying the geological characteristics of the earth's surface from outer space for economic purposes.

1980 April 9

13:38 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Soyuz 35 - . Call Sign: Dnepr (Dnieper ). Crew: Popov, Ryumin. Backup Crew: Andreyev, Zudov. Payload: Soyuz 7K-T s/n 51. Mass: 6,800 kg (14,900 lb). Nation: Russia. Agency: MOM. Program: Salyut 6. Class: Manned. Type: Manned spacecraft. Flight: Soyuz 35. Spacecraft Bus: Soyuz. Spacecraft: Soyuz 7K-T. Duration: 55.06 days. Decay Date: 1980-06-03 . USAF Sat Cat: 11753 . COSPAR: 1980-027A. Apogee: 247 km (153 mi). Perigee: 197 km (122 mi). Inclination: 51.60 deg. Period: 88.90 min. Manned two crew. Docked with Salyut 6. Carried crew comprising L I Popov and V V Ryumin to the Salyut-6 station to carry out scientific and technical research and experiments..

1981 March 12

19:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Soyuz T-4 - . Call Sign: Foton (Photon ). Crew: Kovalyonok, Savinykh. Backup Crew: Andreyev, Zudov. Payload: Soyuz T s/n 10L. Mass: 6,850 kg (15,100 lb). Nation: Russia. Agency: MOM. Program: Salyut 6. Class: Manned. Type: Manned spacecraft. Flight: Soyuz T-4. Spacecraft Bus: Soyuz. Spacecraft: Soyuz T. Duration: 74.73 days. Decay Date: 1981-05-26 . USAF Sat Cat: 12334 . COSPAR: 1981-023A. Apogee: 237 km (147 mi). Perigee: 201 km (124 mi). Inclination: 51.60 deg. Period: 88.90 min. Manned two crew. Docked with Salyut 6. Transported to the Salyut-6 orbital station cosmonauts V V Kovalenok and V P Savinykh to carry out repairs and preventive maintenance and scientific and technical investigations and experiments..