Encyclopedia Astronautica
ST-735


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).

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