 | DS-U2-M
|
Class: Technology. Type: Navigation. Destination: Maximum Payload Orbit. Nation: Ukraine. Agency: MO SSSR. Manufacturer: Yuzhnoye. Development tests of atomic clocks. Typical orbit: 220 km x 2126 km at 48 degrees inclination. Mass: 260 kg (570 lb).
DS-U2-M Chronology - 1965 November 26 - Cosmos 97 - Program: DS. Launch Site: Kapustin Yar. Launch Complex: LC86/1. Launch Vehicle: Kosmos 2. Mass: 267 kg (588 lb). Perigee: 214 km (132 mi). Apogee: 2,144 km (1,332 mi). Inclination: 48.40 deg. Period: 108.90 min.
Development tests of atomic clocks.
- 1967 March 3 - Cosmos 145 - Program: DS. Launch Site: Kapustin Yar. Launch Complex: LC86/1. Launch Vehicle: Kosmos 2. Mass: 250 kg (550 lb). Perigee: 226 km (140 mi). Apogee: 2,107 km (1,309 mi). Inclination: 48.40 deg. Period: 108.70 min.
Development tests of atomic clocks.
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.
- Agapov, V, Novosti Kosmonavtiki, "K zapusku pervovo ISZ serii 'DS'", 1997, Issue 6.
Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.
© Mark Wade, 1997 - 2008 except where otherwise noted.
|
 | DS-U2-M
Credit- Yuzhnoye |
 | DS-U2-M2
Other satellites in the DS-U2-M series had a similar appearance....
Other satellites in the DS-U2-M series had a similar appearance. |
|
