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astronautix.com Osumi


Class: Technology. Nation: Japan. Agency: Japan(Lambda 4S 5).

Engineering test for the launching of scientific satellites. Injection point 29.7 N, 145.8 E.


Specification

Total Mass: 12 kg.


Osumi Chronology


11 February 1970 Ohsumi 5 Launch Site: Kagoshima . Launch Vehicle: L-4S. Mass: 12 kg. Perigee: 323 km. Apogee: 2,440 km. Inclination: 31.0 deg.

Engineering tests. Engineering test for the launching of scientific satellites. Injection point 29.7 N, 145.8 E



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Last update 12 March 2001.
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© Mark Wade, 2001 .