Japanese sounding rocket. Single stage vehicle.
Status: Retired 1974.
Gross mass: 2,300 kg (5,000 lb).
Height: 7.00 m (22.90 ft).
Diameter: 0.50 m (1.64 ft).
Apogee: 200 km (120 mi).
First Launch: 1969.09.15.
Last Launch: 1974.02.01.
Number: 10 .
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
-
NASDA Japanese agency overseeing development of rockets, spacecraft, and rocket engines. National Space Development Agency, 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
-
JCR-1 Solid propellant rocket stage. Loaded mass 700 kg. More...
JCR Chronology
1969 September 15 - .
01:40 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
LV Family:
S.
Launch Vehicle:
JCR.
LV Configuration: JCR-1.
- Test mission - .
Nation: Japan. Agency: NASDA. Apogee: 200 km (120 mi).
1969 September 16 - .
06:40 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
LV Family:
S.
Launch Vehicle:
JCR.
LV Configuration: JCR-2.
- Test mission - .
Nation: Japan. Agency: NASDA. Apogee: 200 km (120 mi).
1970 February 1 - .
01:00 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
LV Family:
S.
Launch Vehicle:
JCR.
LV Configuration: JCR-3.
- Test mission - .
Nation: Japan. Agency: NASDA. Apogee: 200 km (120 mi).
1970 February 4 - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
LV Family:
S.
Launch Vehicle:
JCR.
LV Configuration: JCR-4.
- Test mission - .
Nation: Japan. Agency: NASDA. Apogee: 200 km (120 mi).
1971 February 1 - .
01:30 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
LV Family:
S.
Launch Vehicle:
JCR.
LV Configuration: JCR-5.
- Test mission - .
Nation: Japan. Agency: NASDA. Apogee: 200 km (120 mi).
1971 September 17 - .
06:40 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
LV Family:
S.
Launch Vehicle:
JCR.
LV Configuration: JCR-6.
- Test mission - .
Nation: Japan. Agency: NASDA. Apogee: 200 km (120 mi).
1972 February 6 - .
06:35 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
LV Family:
S.
Launch Vehicle:
JCR.
LV Configuration: JCR-7.
- Test mission - .
Nation: Japan. Agency: NASDA. Apogee: 200 km (120 mi).
1973 February 7 - .
01:50 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
LV Family:
S.
Launch Vehicle:
JCR.
LV Configuration: JCR-8.
- Test mission - .
Nation: Japan. Agency: NASDA. Apogee: 200 km (120 mi).
1973 September 7 - .
01:40 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
LV Family:
S.
Launch Vehicle:
JCR.
LV Configuration: JCR-9.
- Test mission - .
Nation: Japan. Agency: NASDA. Apogee: 200 km (120 mi).
1974 February 1 - .
06:30 GMT - .
Launch Site:
Tanegashima.
Launch Complex:
Tanegashima T.
LV Family:
S.
Launch Vehicle:
JCR.
LV Configuration: JCR-10.
- Test mission - .
Nation: Japan. Agency: NASDA. Apogee: 200 km (120 mi).
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