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S-300 ISAS
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Sounding rocket. Year: 1966. Family: Other Suborbital Vehicles. Country: Japan. Single stage vehicle consisting of 1 x S-300 Manufacturer: ISAS. Launches: 4. Failures: 2. Success Rate: 50.00%. First Launch Date: 1966-11-04. Last Launch Date: 1969-09-08. Launch data is: complete. Apogee: 160 km (90 mi). Total Mass: 600 kg (1,320 lb). Total Length: 6.00 m (19.60 ft).
S-300 ISAS Chronology 1966 November 4 - 02:05 GMT - Launch Site: Kagoshima. Launch Vehicle: S-300 ISAS. Model: S-300. LV Configuration: S-300 PT-300-1. - Test mission Nation: Japan. Agency: ISAS. Apogee: 160 km (90 mi). References: 1145.
1969 January 9 - Launch Site: Kagoshima. Launch Vehicle: S-300 ISAS. Model: S-300. LV Configuration: S-300 S-300-1. FAILURE: Failure. - Aeronomy mission Nation: Japan. Agency: ISAS. References: 1592.
1969 August 24 - Launch Site: Kagoshima. Launch Vehicle: S-300 ISAS. Model: S-300. LV Configuration: S-300 S-300-2. - Test mission Nation: Japan. Agency: ISAS. Apogee: 160 km (90 mi). References: 1592.
1969 September 8 - 10:20 GMT - Launch Site: Kagoshima. Launch Vehicle: S-300 ISAS. Model: S-300. LV Configuration: S-300 S-300-3. FAILURE: Failure. - Aeronomy mission Nation: Japan. Agency: ISAS. Apogee: 10 km (6 mi). References: 1592.
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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