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ST-735
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Test vehicle. Year: 1994. Family: Other Suborbital Vehicles. Country: Japan. 2 stage vehicle consisting of 1 x ST-735 + 1 x ST-735 stage 2 Manufacturer: ISAS. Launches: 2. First Launch Date: 1984-01-17. Last Launch Date: 1994-09-16. Launch data is: complete. Apogee: 120 km (70 mi). Total Mass: 7,400 kg (16,300 lb). Core Diameter: 0.74 m (2.42 ft). Total Length: 4.60 m (15.00 ft).
ST-735 Chronology 1984 January 17 - Launch Site: Kagoshima. Launch Vehicle: ST-735. LV Configuration: ST-735 ST-735-1. - SRB Sep test mission Nation: Japan. Agency: ISAS. Apogee: 50 km (31 mi). References: 847.
1994 September 16 - 04:00 GMT - Launch Site: Kagoshima. Launch Vehicle: ST-735. LV Configuration: ST-735 ST-735-2. - FIH test mission Nation: Japan. Agency: ISAS. Apogee: 118 km (73 mi). References: 1559.
Bibliography and Further Reading - McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Jonathan McDowell's complete on-line listing of all objects orbited and over 20,000 rocket launches Accessed at: http://www.planet4589.org/jsr.html.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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