Encyclopedia Astronautica
DS-MG



cosmosxy.jpg
Cosmos spacecraft
Cosmos spacecraft of DS series
Credit: © Mark Wade
dsmg1.jpg
DS-MG
Credit: Yuzhnoye
dsmg.jpg
DS-MG
Other satellites in the DS-M series had a similar appearance.
Ukrainian technology satellite. 2 launches, 1964.03.18 (Cosmos 26) to 1964.10.24 (Cosmos 49). Payload developed by VNIIEM to test electric gyrodyne orientation systems. Also studied magnetosphere of the earth.

Gross mass: 360 kg (790 lb).
First Launch: 1964.03.18.
Last Launch: 1964.10.24.
Number: 2 .

More... - Chronology...


Associated Countries
See also
  • DS The DS ('Dnepropetrovsk Sputnik') small satellite bus was developed by Yangel's OKB-586 / KB Yuzhnoye in the Ukraine for launch by the same bureau's Kosmos launch vehicles. They were used for a wide range of military and scientific research; component proving tests; and as radar, ASAT, and ABM targets. More...
  • Kosmos 2 In 1960 the Soviet government decreed development of a lightweight launch vehicle for launch of payloads not requiring R-7 family of boosters. A modification of the R-12 IRBM was selected as the first stage; a new high-performance second stage was developed using a unique Lox/UDMH propellant combination. After two failures, the first successful flight was on March 16, 1962. More...

Associated Launch Vehicles
  • Kosmos 2 Ukrainian orbital launch vehicle. In 1960 the Soviet government decreed development of a lightweight launch vehicle for launch of payloads not requiring R-7 family of boosters. A modification of the R-12 IRBM was selected as the first stage; a new high-performance second stage was developed using a unique Lox/UDMH propellant combination. After two failures, the first successful flight was on March 16, 1962. More...
  • Kosmos 63S1 Ukrainian orbital launch vehicle. The 63S1 initial production version was used through May 1966 for a total of 40 launches, of which 12 were failures. It was succeeded by the 63S1M prototype for the 11K63 production space launcher. More...

Associated Manufacturers and Agencies
  • Yuzhnoye Ukrainian manufacturer of rockets, spacecraft, and rocket engines. Yangel Design Bureau, Dnepropetrovsk, Ukraine. More...

Associated Programs
  • DS DS ('Dnepropetrovsk Sputnik') were small satellites built by Yangel's OKB-586 / KB Yuzhnoye in the Ukraine for launch by the same KB's Kosmos launch vehicles. They were used for a wide range of military and scientific research and component proving tests. More...

Bibliography
  • McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: here.
  • JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. Web Address when accessed: here.
  • Agapov, V, "K zapusku pervovo ISZ serii 'DS'", Novosti Kosmonavtiki, 1997, Issue 6.

Associated Launch Sites
  • Kapustin Yar Russia's first missile test range and used for satellite launches of smaller Kosmos vehicles. V-2's launched from here in 1946 were the first ballistic missiles fired on Soviet territory. It was greatly expanded as the test site for innumerable Soviet intermediate and short range missile projects in the 1950's.. Kapustin Year was also headquarters of the first operational R-1/R-2 units, 1950-1953, and later a base for 12 operational R-14 missile launchers. Kapustin Yar was known to have been used for over 3519 major launches from 1946 to 2007. More...

DS-MG Chronology


1964 March 18 - . 15:07 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar Mayak-2. LV Family: Kosmos 2. Launch Vehicle: Kosmos 63S1.
  • Cosmos 26 - . Payload: DS-MG s/n 1. Mass: 365 kg (804 lb). Nation: USSR. Agency: MO. Program: DS. Class: Technology. Type: Navigation technology satellite. Spacecraft: DS-MG. Completed Operations Date: 1964-04-01 . Decay Date: 1964-09-28 . USAF Sat Cat: 766 . COSPAR: 1964-013A. Apogee: 376 km (233 mi). Perigee: 268 km (166 mi). Inclination: 48.9000 deg. Period: 91.00 min. Summary: Payload developed by VNIIEM to test electric gyrodyne orientation systems. Also obtained radiation data..

1964 October 24 - . 05:16 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar Mayak-2. LV Family: Kosmos 2. Launch Vehicle: Kosmos 63S1.
  • Cosmos 49 - . Payload: DS-MG s/n 2. Mass: 355 kg (782 lb). Nation: USSR. Agency: MO. Program: DS. Class: Technology. Type: Navigation technology satellite. Spacecraft: DS-MG. Completed Operations Date: 1964-11-09 . Decay Date: 1965-08-21 . USAF Sat Cat: 913 . COSPAR: 1964-069A. Apogee: 472 km (293 mi). Perigee: 260 km (160 mi). Inclination: 48.9000 deg. Period: 91.90 min. Summary: Payload developed by VNIIEM to test electric gyrodyne orientation systems. Also studied measured Earth infrared and ultraviolet flux..

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