Japanese sounding rocket. Derivative of S-310.
Status: Retired 1966.
Gross mass: 700 kg (1,540 lb).
Height: 6.00 m (19.60 ft).
Diameter: 0.31 m (1.01 ft).
Apogee: 5.00 km (3.10 mi).
First Launch: 1966.04.28.
Last Launch: 1966.08.06.
Number: 3 .
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
-
ISAS Japanese agency overseeing development of rockets, spacecraft, and rocket engines. Institute of Space and Astronautical Science, Japan. More...
Associated Launch Sites
-
Kagoshima Japanese launch center for solid fueled sounding rockets and satellite launchers. Limited to two months a year due to disturbance of local fisheries. More...
Associated Stages
BT-310 Chronology
1966 April 28 - .
02:00 GMT - .
Launch Site:
Kagoshima.
LV Family:
S.
Launch Vehicle:
BT-310.
LV Configuration: BT-310 BT-310-1.
- Test mission - .
Nation: Japan. Agency: ISAS. Apogee: 1.00 km (0.60 mi).
1966 April 29 - .
00:00 GMT - .
Launch Site:
Kagoshima.
LV Family:
S.
Launch Vehicle:
BT-310.
LV Configuration: BT-310 BT-310-2.
- Test mission - .
Nation: Japan. Agency: ISAS. Apogee: 1.00 km (0.60 mi).
1966 August 6 - .
02:00 GMT - .
Launch Site:
Kagoshima.
LV Family:
S.
Launch Vehicle:
BT-310.
LV Configuration: BT-310 MM-310-1.
- Mu Scale Model test - .
Nation: Japan. Agency: ISAS. Apogee: 2.00 km (1.20 mi).
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