 | DS-2 Credit - Yuzhnoye
| Class: Technology. Destination: Maximum Payload Orbit. Nation: Ukraine. Manufacturer: Yuzhnoye. A decision was made after two unsuccessful launches of the DS-1 to create a simplified DS-2 spacecraft based on the equipment and structural elements of DS-1 spacecraft. The cylindrical section for mission avionics was completely omitted. Typical orbit: 207 km x 649 km at 49 degrees inclination. Mass: 315 kg (694 lb). Associated Launch Vehicle: Kosmos 63S1.
DS-2 Chronology
- 1962 March 16 - Cosmos 1 - Program: DS. Launch Site: Kapustin Yar. Launch Vehicle: Kosmos 2. Mass: 47 kg (103 lb). Perigee: 207 km (128 mi). Apogee: 649 km (403 mi). Inclination: 49.00 deg. Period: 93.10 min.
After five months of further work and tests to improve the reliability of the second stage, Yangel's team felt it was ready to again attempt a launch of the 63S1 booster. 63S1 s/n 6LK put a DS-2 satellite into orbit, which conducted studies of the ionosphere. This was the first successful launch of the Kosmos 63S1 launch vehicle. A decision was made after two unsuccessful launches of the DS-1 to create a simplified DS-2 spacecraft based on the equipment and structural elements of DS-1 spacecraft. The cylindrical section for mission avionics was completely omitted.
Bibliography:- McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: http://www.planet4589.org/jsr.html.
- JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. Web Address when accessed: http://msl.jpl.nasa.gov/home.html.
- Zak, Anatoly, Spaceflight, "Cosmos Launcher", 1996, Volume 38, page 416.
- Agapov, V, Novosti Kosmonavtiki, "K zapusku pervovo ISZ serii 'DS'", 1997, Issue 6.
- Siddiqi, Asif A, The Soviet Space Race With Apollo, University Press of Florida, 2003.
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