Japanese sounding rocket. Single stage vehicle.
Status: Retired 1969.
Gross mass: 100 kg (220 lb).
Height: 2.90 m (9.50 ft).
Diameter: 0.17 m (0.55 ft).
Apogee: 85 km (52 mi).
First Launch: 1969.02.07.
Last Launch: 1969.02.08.
Number: 3 .
More... - Chronology...
Associated Countries
See also
-
S Series of Japanese single-stage sounding rockets designed for low-cost observations of the ionosphere. More...
Associated Manufacturers and Agencies
-
Mitsubishi Japanese manufacturer of rockets, spacecraft, and rocket engines. Mitsubishi Electric Corp, Japan. More...
Associated Launch Sites
-
Tanegashima Japan's main launch site for he larger N and H launch vehicles. In use for sounding rockets from 1967 and orbital launches from 1975. As of 2007 over 140 major launches had been made from the site. More...
Associated Stages
-
S-C-1 Solid propellant rocket stage. Loaded mass 100 kg. More...
S-C Chronology
1969 February 7 - .
06:30 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
LV Family:
S.
Launch Vehicle:
S-C.
LV Configuration: S-C SC-3.
- Test mission - .
Nation: Japan. Agency: STA. Apogee: 85 km (52 mi).
1969 February 8 - .
01:30 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
LV Family:
S.
Launch Vehicle:
S-C.
LV Configuration: S-C SC-4.
- Test mission - .
Nation: Japan. Agency: STA. Apogee: 85 km (52 mi).
1969 February 8 - .
06:30 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
LV Family:
S.
Launch Vehicle:
S-C.
LV Configuration: S-C SC-1.
- Test mission - .
Nation: Japan. Agency: STA. Apogee: 85 km (52 mi).
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