1972

February 25. "Kosmos 475". Military navigation satellite. Perigee: 961 km. Apogee: 993 km. Inclination: 74.0 deg. Period: 104.6 min. March 1. "Kosmos 476" ("Tselina-D" N° 3). Perigee: 379 km. Apogee: 388 km. Inclination: 81.2 deg. Period: 92.2 min. March 4. "Kosmos 477" ("Zenit-2M") Area survey photo reconnaissance satellite. Perigee: 202 km. Apogee: 306 km. Inclination: 72.9 deg. Period: 89.6 min.  Duration: 12 days. March 15. "Kosmos 478" ("Zenit-4M") High resolution photo reconnaissance satellite Perigee: 176 km. Apogee: 282 km. Inclination: 65.0 deg. Period: 89.0 min. Duration: 13 days. March 22. "Kosmos 479" ("Tselina-O" ). ELINT satellite. Perigee: 517 km. Apogee: 537 km. Inclination: 74.0 deg. Period: 95.2 min. March 25. "Kosmos 480" ("Sfera'") Perigee: 1,170 km. Apogee: 1,196 km. Inclination: 83.0 deg. Period: 109.1 min.  March 26. "Kosmos 481" Perigee: 277 km. Apogee: 496 km. Inclination: 70.0 deg. Period: 92.3 min. Completed Operations Date: 3 September 1972. April 4. "MAS-1", the French spacecraft was launched from "Plesetsk" cosmodrome ( with "Molniya-1" satellite simultaneously). April 5. "Molniya 2-05". Continued operation of the long-range telephone and telegraph radio-communication system within the Soviet Union and transmission of USSR central television programs to stations in the "Orbita" and participating international networks (international coope ration scheme). April 12. "Kosmos 553". April 19. "Kosmos 554" ("Zenith-4MK"). High resolution photo reconnaissance satellite; returned film capsule; maneuverable; exploded in orbit. April 19, Kapustin Yar.  "Interkosmos 9". Solar radition monitor. Name is "Intercosmos Copernicus 500". Investigation of solar radio-frequency radiation and the characteristics of the earth's ionosphere. April 25. "Kosmos 555" ("Zenith-2M"). Area survey photo reconnaissance satellite; returned film capsule; separated science capsule. May 5. "Kosmos 556" ("Zenith-4MK"). High resolution photo reconnaissance satellite. May 14, Cape Canaveral, USA. "Skylab 1". First and only US space station to date. Project began life as Apollo Orbital Workshop - outfitting of an S-IVB stage with docking adapter with equipment launched by several subsequent S-1B launches. Curtailment of the Apollo moon landings meant that surplus Saturn V's were available, so the pre-equipped, five times heavier, and much more capable Skylab resulted.   An unexpected telemetry indication of meteoroid shield deployment and solar array wing 2 beam fairing separation was received 1 minute and 3 seconds after liftoff. However, all other systems of the OWS appeared normal, and the OWS was inserted into a near-circular Earth orbit of approximately 435 km altitude. The payload shroud was jettisoned, and the ATM with its solar array was deployed as planned during the first orbit. Deployment of the Workshop solar array and the meteoroid shield was not successful. In fact the external solar/meteoroid shield had ripped off 63 seconds into ascent, tearing away one solar panel wing and debris jamming the remaining panel. Without shield temperatures soared in station. Repairs by crews led to virtually all mission objectives being met. Following the final manned phase of the Skylab mission, ground controllers performed some engineering tests of certain Skylab systems--tests that ground personnel were reluctant to do while men were aboard. Results from these tests helped to determine causes of failures during the mission and to obtain data on long term degradation of space systems. Upon completion of the engineering tests, Skylab was positioned into a stable attitude and systems were shut down. It was expected that Skylab would remain in orbit eight to ten years. It was to have been visited by an early shuttle mission, reboosted into a higher orbit, and used by space shuttle crews. But delays in the first flight of the shuttle made this impossible. On July 11, 1979, Skylab disintegrated when it re-entered the earth's atmosphere after a worldwide scare over its pending crash. The debris stretched from the south-east Indian Ocean into Western Australia. May 17. "Kosmos 558" Investigation of the upper atmosphere and outer space. May 18. "Kosmos 559" ("Zenith-4MK"). First flight of "Soyuz-U" launch vehicle. High resolution photo reconnaissance satellite. May 23. "Kosmos 560" ("Zenith-4M"). High resolution photo reconnaissance satellite. May 25. "Kosmos 561" ("Zenith-2M"). Area survey photo reconnaissance satellite; returned film capsule; separated gamma ray telescope experiment capsule. May 29. "Meteor 1-15". Acquisition of meteorological information needed for use by the weather service. June 3. Cosmonaut Vladimir Nikolaevich Benderov dies at age of 48 -- Crash in Tu-144. June 5 Kosmos 562".  June 6. "Kosmos 563" ("Zenith-4M"). High resolution photo reconnaissance satellite. June 8. "Kosmos 564"-"Kosmos 571"  ("Strela-1M"). Eight satellites launched by a single carrier rocket. June 20. "Kosmos 574". Military navigation satellite. June 21. "Kosmos 575". Area survey photo reconnaissance satellite. June 26. "Tselina-O" failure. June 27. "Kosmos 576" ("Zenith-4MK"). Military topography satellite. July 4. "Zenith-4M".High resolution photo reconnaissance satellite. July 11. "Molniya 2-06". Continued operation of the long-range telephone and telegraph radio-communication system within the Soviet Union and transmission of USSR central television programs to stations in the "Orbita" and participating international networks (international coope ration scheme). July 19. Cosmonaut Vasily Dmitriyevich Shcheglov dies at age of 33 - Natural causes.  July 25. "Kosmos 577" ("Zenith-4M"). High resolution photo reconnaissance satellite.  August 1. "Kosmos 578" ("Zenith-2M"). Area survey photo reconnaissance satellite.

   

The MAS flights were part of the continuing Franco-Soviet cooperative space effort, which, with the possible exception of the "Apollo" - "Soyuz" test Program, is the most extensive cooperative space effort involving the USSR and a Western industrial democracy. The two MAS missions were small piggyback payloads added to "Molniya" communications satellite launches. Called "STRET 1" by the French, this mission was designed to test various types of solar cells for future French and Soviet spacecraft. "STRET 2" was orbited in order to conduct engineering tests of materials designed to provide thermal protection for future payloads. Teflon, kenton and other substances were evaluated.

   
FRANCE.JPG (15433 bytes)
The first foreigners (French specialists) on the streets of  the "Secret town".

This page is currently under development.
SS © 2003