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Test vehicle. Year: 1989. Family: Other Suborbital Vehicles. Country: USA. Single stage vehicle consisting of 1 x AMROC IRR Manufacturer: AMROC. Launches: 1. Failures: 1. Success Rate: 0.00%. First Launch Date: 1989-10-05. Last Launch Date: 1989-10-05. Launch data is: complete. Apogee: 100 km (60 mi). Liftoff Thrust: 315.000 kN (70,814 lbf). Total Mass: 12,200 kg (26,800 lb). Core Diameter: 1.29 m (4.23 ft). Total Length: 17.70 m (58.00 ft).
AMROC IRR Chronology 1989 October 5 - 17:28 GMT - Launch Site: Vandenberg. Launch Complex: BMRS. Launch Pad: BMRSA3. Launch Vehicle: AMROC IRR. LV Configuration: AMROC IRR SET-1. FAILURE: Failure. - Test mission Nation: USA. Agency: AMROC. References: 1812.
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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