Grom (original) (raw)
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Grom
Russian orbital launch vehicle derived from R-39 SLBM.
Status: Active. First Launch: 1996-01-01. Last Launch: 2003-12-11. Number: 4 . Thrust: 2,060.00 kN (463,100 lbf). Gross mass: 84,000 kg (185,000 lb). Height: 16.00 m (52.00 ft). Diameter: 2.40 m (7.80 ft). Apogee: 1,000 km (600 mi).
Maximum range: 8,300 km (5,100 mi).
Family: orbital launch vehicle, submarine-launched. Country: Russia. Launch Sites: Nenoksa. Stages: Grom-2, 15D305, Rif-3. Agency: Makeyev bureau.
1996 - . Launch Site: Nenoksa. LV Family: R-39. Launch Vehicle: Grom. FAILURE: Failure.
1997? - . Launch Site: Nenoksa. LV Family: R-39. Launch Vehicle: Grom. FAILURE: Failure.
1997 November 19 - . Launch Site: Nenoksa. LV Family: R-39. Launch Vehicle: Grom. FAILURE: Failure.
2003 December 11 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: TK-208. LV Family: R-39. Launch Vehicle: Grom.
- RSM-52M / R-39UTTKh / Grom test - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E..
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