Japanese test vehicle. Two stage vehicle consisting of 1 x ST-735 + 1 x ST-735 stage 2
Gross mass: 7,400 kg (16,300 lb).
Height: 4.60 m (15.00 ft).
Diameter: 0.74 m (2.42 ft).
Apogee: 120 km (70 mi).
First Launch: 1984.01.17.
Last Launch: 1994.09.16.
Number: 2 .
More... - Chronology...
Associated Countries
See also
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
ST-735 Chronology
1984 January 17 - .
Launch Site:
Kagoshima.
Launch Complex:
Kagoshima L.
Launch Pad: K?.
LV Family:
SB-735.
Launch Vehicle:
ST-735.
LV Configuration: ST-735-1 ST-735-1.
- SRB Sep test - .
Nation: Japan. Agency: ISAS. Apogee: 50 km (31 mi).
1994 September 16 - .
04:00 GMT - .
Launch Site:
Kagoshima.
Launch Complex:
Kagoshima L.
Launch Pad: K?.
LV Family:
SB-735.
Launch Vehicle:
ST-735.
LV Configuration: ST-735 ST-735-2.
- FIH test - .
Nation: Japan. Agency: ISAS. Apogee: 118 km (73 mi).
Home - Browse - Contact
© / Conditions for Use
