AMROC IRR (original) (raw)

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AMROC IRR

Part of AMROC

American low cost orbital launch vehicle. Single stage vehicle.

AKA: IRR. Status: Retired 1989. First Launch: 1989-10-05. Last Launch: 1989-10-05. Number: 1 . Thrust: 315.00 kN (70,814 lbf). Gross mass: 12,200 kg (26,800 lb). Burn time: 70 s. Height: 17.70 m (58.00 ft). Diameter: 1.29 m (4.23 ft). Apogee: 100 km (60 mi).

Family: LCLVs, low cost, orbital launch vehicle. Country: USA. Engines: H1500. Launch Sites: Vandenberg, Vandenberg 576A3. Agency: eAc.

1989 October 5 - . 17:28 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: AMROC. Launch Vehicle: AMROC IRR. FAILURE: Failure.

Test mission - . Nation: USA. Agency: AMROC. Apogee: 0 km (0 mi).

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