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Storm-2
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Test vehicle. Year: 1997. Family: Minuteman. Country: USA. Single stage vehicle consisting of 1 x SR19AJ1 Manufacturer: OSC. Launches: 5. Failures: 1. Success Rate: 80.00%. First Launch Date: 1997-01-29. Last Launch Date: 2002-04-25. Launch data is: continuing. Apogee: 150 km (90 mi). Liftoff Thrust: 267.000 kN (60,023 lbf). Total Mass: 8,000 kg (17,600 lb). Core Diameter: 1.32 m (4.33 ft). Total Length: 9.90 m (32.40 ft).
Storm-2 Chronology 1997 January 29 - Launch Site: White Sands. Launch Complex: LC32. Launch Vehicle: Storm-2. FAILURE: Failure. - MTTV/MTD-2 PAC Targ Target mission Nation: USA. Agency: USA SSDC. Apogee: 10 km (6 mi). References: 1876.
1997 September 24 - Launch Site: White Sands. Launch Complex: LC32. Launch Vehicle: Storm-2. - MTTV-4/Patriot Targ Target mission Nation: USA. Agency: USA SSDC. Apogee: 110 km (60 mi). References: 1823.
1998 September 24 - 12:50 GMT - Launch Site: White Sands. Launch Complex: LC32. Launch Vehicle: Storm-2. - MTTV/MTD-3 Target mission Nation: USA. Agency: USA/OSC. Apogee: 180 km (110 mi). References: 1823.
2000 October 14 - Launch Site: Fort Wingate. Launch Complex: LC96. Launch Vehicle: Storm-2. LV Configuration: Storm-2 MTTV. - PAC-3 DT-6 Target mission Nation: USA. Agency: USA SSDC. Apogee: 104 km (64 mi). References: 1908.
2002 Apr 25 1300? - 13:00 GMT - Launch Site: White Sands. Launch Vehicle: Storm-2. - PAC-3 OT/DT-4 Target mission Nation: USA. Agency: USA SSDC. Apogee: 100 km (60 mi). References: 1849.
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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