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Grom
Part of R-39
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.
- Test mission - .
Nation: Russia.
Agency: RVSN,
VMF.
Apogee: 0 km (0 mi).
1997? - .
Launch Site:
Nenoksa.
LV Family:
R-39.
Launch Vehicle:
Grom.
FAILURE: Failure.
- Test mission - .
Nation: Russia.
Agency: RVSN,
VMF.
Apogee: 0 km (0 mi).
1997 November 19 - .
Launch Site:
Nenoksa.
LV Family:
R-39.
Launch Vehicle:
Grom.
FAILURE: Failure.
- Test mission - .
Nation: Russia.
Agency: RVSN,
VMF.
Apogee: 0 km (0 mi).
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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