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Barents Sea Launch Area

Site · Russia

Original archive entry. The text, images and links below are kept as they were written.

Barents Sea
Barents Sea
Credit: © Mark Wade

Submarine-launched ballistic missile launch area.

Subtopics

Country
Russia
Spacecraft
Parus, Tubsat, Kompas

Chronology

142 events

1965 May 19

13:00 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-170. Launch Vehicle: R-13.
  • Nation: Russia. Agency: RVSN. Apogee: 150 km (90 mi).

1965 May 24

10:00 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: GOLF. Launch Vehicle: R-13.
  • Nation: Russia. Agency: RVSN. Apogee: 150 km (90 mi).

1965 May 25

13:00 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: GOLF. Launch Vehicle: R-13.
  • Nation: Russia. Agency: RVSN. Apogee: 150 km (90 mi).

1965 May 26

13:36 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-170. Launch Vehicle: R-13.
  • Nation: Russia. Agency: RVSN. Apogee: 150 km (90 mi).

1965 May 31

13:30 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: GOLF. Launch Vehicle: R-13.
  • Nation: Russia. Agency: RVSN. Apogee: 150 km (90 mi).

1977 March 18

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1977 March 20

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1984 September 7

07:10 GMT - . Launch Site: Barents Sea Launch Area. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Volna.
  • Caused UFO sighting - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1986 September 1

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: DELTA2. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1990 January 2

19:57 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 84 km (52 mi).

1990 January 2

20:27 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 80 km (49 mi).

1990 January 9

20:10 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 79 km (49 mi).

1990 January 9

20:30 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 76 km (47 mi).

1990 January 16

20:12 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 80 km (49 mi).

1990 January 18

21:00 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 82 km (50 mi).

1990 January 23

20:54 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 80 km (49 mi).

1990 January 25

20:20 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 82 km (50 mi).

1990 February 6

20:00 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 80 km (49 mi).

1990 February 13

20:00 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 80 km (49 mi).

1990 February 20

20:16 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 80 km (49 mi).

1990 February 27

20:04 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 81 km (50 mi).

1990 March 6

19:20 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 77 km (47 mi).

1990 March 13

20:00 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 77 km (47 mi).

1990 March 20

19:40 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 80 km (49 mi).

1990 March 27

19:55 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 80 km (49 mi).

1990 November 2

17:53 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 84 km (52 mi).

1990 November 9

17:00 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 82 km (50 mi).

1990 November 14

16:10 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 81 km (50 mi).

1990 November 21

20:00 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 79 km (49 mi).

1990 November 28

18:46 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 84 km (52 mi).

1990 November 28

21:30 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 80 km (49 mi).

1990 December 4

19:55 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 83 km (51 mi).

1990 December 4

21:15 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 72 km (44 mi).

1990 December 4

22:20 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 72 km (44 mi).

1990 December 11

19:55 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 83 km (51 mi).

1990 December 18

19:55 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 82 km (50 mi).

1990 December 25

20:40 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. LV Family: M-100. Launch Vehicle: M-100B.
  • Nation: Russia. Apogee: 82 km (50 mi).

1995 June 6

22:10 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: KALMAR. LV Family: R-29. Launch Vehicle: Volna.
  • Volan? - . Nation: Russia. Agency: VMF. Apogee: 1,270 km (780 mi).

1996 July 15

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: DELTA3. LV Family: R-29. Launch Vehicle: Vysota.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1996 July 15

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: DELTA4. LV Family: R-29. Launch Vehicle: Shtil'.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1996 October 3

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Shtil'.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1996 October 23

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 January 15

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: KALMAR. LV Family: R-29. Launch Vehicle: Volna.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1997 March 27

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 27

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 27

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 27

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 27

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 27

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 27

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 27

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 27

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 27

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 28

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 28

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 28

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 28

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 28

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 28

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 28

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 28

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 28

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 28

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 March 28

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 3.00 km (1.80 mi).

1997 December 3

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 3

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 3

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 3

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 3

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 3

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 3

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 3

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 3

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 3

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 3

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 3

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 4

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 4

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 4

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 4

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 4

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 4

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 4

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1997 December 4

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Arms control - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1998 February 19

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: DELTA4. LV Family: R-29. Launch Vehicle: Shtil'.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1998 February 19

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: DELTA4. LV Family: R-29. Launch Vehicle: Shtil'.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1998 July 7

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-407. LV Family: R-29. Launch Vehicle: Shtil'-1.
  • Shtil 1 - . Payload: Shtil-1 instr. package. Nation: Israel. Manufacturer: TuB. Spacecraft: Shtil. Decay Date: 2014-05-08 . USAF Sat Cat: 25391 . COSPAR: 1998-042C. Apogee: 801 km (497 mi). Perigee: 401 km (249 mi). Inclination: 79.00 deg.

    The first satellite launch from a submarine. The Shtil-1 launch vehicle was a converted R-29RM (RSM-54) three stage liquid propellant submarine launched ballistic missile made by the Makeyev design bureau. The satellite payload is placed in the standard R-29RM reentry vehicle. The launch plaform was the K-407 Novomoskovsk, a 667BDRM Delfin class submarine of the Russian Northern Fleet's 3rd Flotilla. Launch was from the Barents Sea at 69.3 degrees N x 35.3 degrees E. The Shtil contained an Israeli instrument package.

  • Tubsat-N - . Mass: 8.00 kg (17.60 lb). Nation: Germany. Agency: VMF. Manufacturer: TuB. Program: Tubsat. Class: Communications. Type: Civilian store-dump communications satellite. Spacecraft: Tubsat. Decay Date: 2002-04-23 . USAF Sat Cat: 25389 . COSPAR: 1998-042A. Apogee: 776 km (482 mi). Perigee: 400 km (240 mi). Inclination: 78.90 deg. Period: 96.40 min.

    The first satellite launch from a submarine. The Shtil-1 launch vehicle was a converted Makeyev R-29RM SLBM. The satellite payload was placed in the standard re-entry vehicle. The launch platform was the K-407 Novomoskovsk, a 667BDRM Delfin class submarine of the Russian Northern Fleet 3rd Flotilla. The launch was made from a firing range in the Barents Sea off the coast of the Kolskiy Peninsula, at 35.3 deg E 69.3 deg N. The payloads were the Tubsat-N and Tubsat-N1 `nanosatellites'. Tubsat-N entered a 400 x 776 km x 78.9 deg orbit. Both carried small store-forward communications payloads used to keep track of transmitters placed on vehicles, migrating animals, and marine buoys. They are owned, operated and built by the Technische Universitat Berlin (TUB). Tubsat-N was the larger of the pair, with dimensions of 32x32x10.4 cm and a mass of 8.5 kg.

  • Tubsat-N1 - . Mass: 3.00 kg (6.60 lb). Nation: Germany. Agency: VMF. Manufacturer: TuB. Program: Tubsat. Class: Communications. Type: Civilian store-dump communications satellite. Spacecraft: Tubsat. Decay Date: 2000-10-21 . USAF Sat Cat: 25390 . COSPAR: 1998-042B. Apogee: 776 km (482 mi). Perigee: 400 km (240 mi). Inclination: 78.90 deg. Period: 96.30 min.

    The dual Tubsat-N/Tubsat-N1 repersented the Technical University of Berlin's first Nanosatellite project. Tubsat-N1 measured 32x32x3.4cm and had a mass of 3 kg. The technology demonstrator satellite provided store and forward communications and conducted attitude control experiments.

1998 August 21

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Volna.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1999 April 1

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Volna.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1999 October 1

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Volna. FAILURE: Failure.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1999 November 17

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

1999 November 17

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Test mission - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

2000 March 27

06:00 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-18. LV Family: R-29. Launch Vehicle: Shtil'.
  • (Kura) - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). Three launches in one day from two submarines..

2000 March 27

09:00 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-18. LV Family: R-29. Launch Vehicle: Shtil'.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2000 April 6

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-496. LV Family: R-29. Launch Vehicle: Volna.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2000 September 12

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-18. LV Family: R-29. Launch Vehicle: Shtil'.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2000 December 27

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-407. LV Family: R-29. Launch Vehicle: Shtil'.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2001 February 16

10:28 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Shtil'.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2001 June 5

11:32 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Shtil'.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2001 July 20

00:31 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-496. LV Family: R-29. Launch Vehicle: Volna.
  • Cosmos 1 Solar Sail Spacecraft test - . Nation: Russia. Agency: VMF. Apogee: 412 km (256 mi).

    Launch delayed from April 26 and July 19 failure. The Russian Navy launched a three-stage R-29R Volna from the submarine Borisoglebsk in the Barents Sea on a suborbital flight. The payload was a joint project between the Planetary Society and NPO Lavochkin's Babakin center, and consisted of a solar sail deployment test with an inflatable reentry shield. The payload failed to separate from the final stage.

2001 September 27

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-29. Launch Vehicle: Shtil'.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2001 September 27

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-29. Launch Vehicle: Shtil'.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2002 July 12

00:58 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-44. LV Family: R-29. Launch Vehicle: Volna.
  • IRDT-2 re-entry vehicle test flight - . Nation: Russia. Agency: VMF. Apogee: 200 km (120 mi).

    The Russian Navy launched the IRDT-2 spacecraft using a surplus R-29R Volna from the submarine K-44 Ryazan. The spacecraft was launched on a suborbital trajectory from the Barents Sea and landed in Kamchatka. After third stage separation the IRDT fired a boost motor to increase its speed and then inflated the first stage of its heat shield.

2002 October 12

09:55 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-20. LV Family: R-29. Launch Vehicle: Shtil'.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2004 February 18

09:30 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-18. LV Family: R-29. Launch Vehicle: Sineva. FAILURE: Failure.
  • Sineva operational test - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi). Failure - destroyed 98 seconds after launch. Launched during a nationwide military exercise..

2004 March 17

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-407. LV Family: R-29. Launch Vehicle: Sineva.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2004 March 17

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-407. LV Family: R-29. Launch Vehicle: Sineva.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2004 June 29

07:25 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-84. LV Family: R-29. Launch Vehicle: Shtil'.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2004 September 8

04:38 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-84. LV Family: R-29. Launch Vehicle: Shtil'.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2004 September 8

07:38 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-496. LV Family: R-29. Launch Vehicle: Volna.
  • Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). SLBM Test - second launch in one day..

2004 September 23

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-208. LV Family: Topol'. Launch Vehicle: Bulava.
  • Bulava cold-launch test - . Nation: Russia. Agency: VMF. Apogee: 1.00 km (0.60 mi). Test of naval version of Topol M ICBM. A mass replica of a the new Bulava SLBM reached under 100 m altitude after being launched from the submerged SSBN Dmitry Donskoi..

2004 December 11

Launch Site: Barents Sea Launch Area. Launch Complex: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-208. LV Family: Topol'. Launch Vehicle: Bulava.
  • Bulava cold-launch test - . Nation: Russia. Agency: VMF. Apogee: 1.00 km (0.60 mi). A mass replica of a the new Bulava SLBM was ejected from its launch tube from the surfaced SSBN Dmitry Donskoi..

2005 June 21

19:46 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-496. LV Family: R-29. Launch Vehicle: Volna. FAILURE: Failure.
  • Cosmos 1 - . Payload: Solnechny Parus. Mass: 103 kg (227 lb). Nation: USA. Agency: Planetary Society. Manufacturer: Lavochkin bureau. Class: Technology. Type: Navigation technology satellite. Spacecraft Bus: KAUR-1. Spacecraft: Parus.

    Launched from SSBN Borisoglebsk. First orbital flight attempt of converted SLBM. Payload was solar sail demonstrator. Delayed from late 2001; March 20 and October 2002; late March, August 28 and October, 2003; February, March, April 6, May 20 and 31, 2005.

2005 August 17

07:06 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-84. LV Family: R-29. Launch Vehicle: Sineva.
  • RSM-54 test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2005 October 6

21:30 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-496. LV Family: R-29. Launch Vehicle: Volna.
  • IRDT-2R re-entry vehicle test flight - . Nation: Germany. Agency: VMF. Apogee: 200 km (120 mi).

    Suborbital test of the Demonstrator inflatable reentry technology test vehicle. The reentry vehicle could not be located in the Kamchatka Peninsula impact zone and was not recovered. Test delayed from the fourth quarter of 2003, then May and October 2004, then July 5, July 8, September 15, September 27, 2005.

2005 October 7

21:30 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-496. LV Family: R-29. Launch Vehicle: Sineva.
  • RSM-54 Test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2006 May 26

18:50 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-84. LV Family: R-29. Launch Vehicle: Shtil'-1.
  • Kompass-2 - . Mass: 80 kg (176 lb). Nation: Russia. Agency: Izmiran. Manufacturer: Makeyev bureau. Class: Technology. Type: Navigation technology satellite. Spacecraft: Kompas. Decay Date: 2011-12-28 . USAF Sat Cat: 29157 . COSPAR: 2006-019A. Apogee: 492 km (305 mi). Perigee: 402 km (249 mi). Inclination: 78.90 deg. Period: 93.50 min.

    Complex Orbital Magneto-Plasma Autonomous Small Satellite. Earthquake research satellite for the Moscow-based IZMIRAN science institute. The satellite carried detectors for electrons, UHF/VHF waves, UV emission and radiation, a radio frequency analyser for electric field waves, and a Mayak ionospheric beacon. Reports indicated that the satellite did not respond to ground commands and that its mission was abandoned.

2006 June 30

06:25 GMT - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-114. LV Family: R-29. Launch Vehicle: Sineva.
  • R-29RM test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2007 December 17

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-114. LV Family: R-29. Launch Vehicle: Shtil'.
  • Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2007 December 25

Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: K-114. LV Family: R-29. Launch Vehicle: Sineva.
  • Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2008 August 1

Launch Site: Barents Sea Launch Area. Launch Platform: K-44. LV Family: R-29. Launch Vehicle: Volna.
  • (Kura) - . Nation: Russia. Apogee: 1,000 km (600 mi).

2008 October 11

Launch Site: Barents Sea Launch Area. Launch Platform: K-114. LV Family: R-29. Launch Vehicle: Sineva.
  • (Pacific) - . Nation: Russia. Apogee: 1,000 km (600 mi).

2008 October 12

Launch Site: Barents Sea Launch Area. Launch Platform: K-84. LV Family: R-29. Launch Vehicle: Shtil'.
  • (Kura) - . Nation: Russia. Apogee: 1,000 km (600 mi).

2008 November 28

Launch Site: Barents Sea Launch Area. Launch Platform: TK-208. LV Family: Topol'. Launch Vehicle: Bulava.

2008 December 23

03:00 GMT - . Launch Site: Barents Sea Launch Area. Launch Platform: TK-208. LV Family: Topol'. Launch Vehicle: Bulava.
  • RV-1 - . Nation: Russia. Agency: VMF. Apogee: 100 km (60 mi).

2009 November 1

Launch Site: Barents Sea Launch Area. Launch Platform: K-117. LV Family: R-29. Launch Vehicle: Sineva.
  • Sineva - . Nation: Russia. Agency: VMF. Operational test.

2010 March 4

04:50 GMT - . Launch Site: Barents Sea Launch Area. Launch Platform: K-114. LV Family: R-29. Launch Vehicle: Sineva.
  • Sineva 4 RV's - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). Operational test launch.

2010 August 6

15:15 GMT - . Launch Site: Barents Sea Launch Area. Launch Platform: K-114. LV Family: R-29. Launch Vehicle: Sineva.
  • RV x4 - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). Operational test..

2010 August 6

15:15 GMT - . Launch Site: Barents Sea Launch Area. Launch Platform: K-114. LV Family: R-29. Launch Vehicle: Sineva.
  • RV x4 - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). Operational test..

2010 October 28

10:30 GMT - . Launch Site: Barents Sea Launch Area. Launch Platform: K-117. LV Family: R-29. Launch Vehicle: Sineva.
  • RV x 4 - . Nation: Russia. Apogee: 1,000 km (600 mi). Operational test..

2011 April 26

Launch Site: Barents Sea Launch Area. Launch Platform: K-84. LV Family: R-29. Launch Vehicle: Sineva.
  • Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). Operational test.

2011 May 20

Launch Site: Barents Sea Launch Area. Launch Platform: K-84. LV Family: R-29. Launch Vehicle: Layner.
  • 4 x RV - . Nation: Russia. Operational test..
  • Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2011 July 27

Launch Site: Barents Sea Launch Area. Launch Platform: K-84. LV Family: R-29. Launch Vehicle: Sineva.
  • RV x ? - . Nation: Russia. Apogee: 1,000 km (600 mi). Test mission. Launched from the Barents Sea to the Kura test range..

2011 September 29

Launch Site: Barents Sea Launch Area. Launch Platform: K-114. LV Family: R-29. Launch Vehicle: Layner.
  • Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).
  • 10 RVs - . Nation: Russia. Apogee: 1,000 km (600 mi). R&D mission. Second test flight of the R-29MU2.1 Layner missile from submarine K-114 Tula. The R-29MU2.1 is a version of the R-29MU2 Sineva missile but carrying up to 10 reentry vehicles..

2013 October 30

Launch Site: Barents Sea Launch Area. Launch Pad: K-117. Launch Platform: K-117. LV Family: R-29. Launch Vehicle: Sineva.
  • RV - . Nation: Russia. Apogee: 1,000 km (600 mi).

    Launched from a sub in the Barents Sea to Kura. One of a series of missiles launched on the same day as part of a large scale Russian military exercise. One Iskander-M and three Tochka-U short range missiles were also launched from Kapustin Yar to unknown targets

2014 May 8

Launch Site: Barents Sea Launch Area. Launch Pad: K-114. Launch Platform: K-114. LV Family: R-29. Launch Vehicle: Shtil'.
  • Shtil' RV - . Nation: Russia. Apogee: 1,000 km (600 mi). Military Exercise.

2014 October 29

17:27 GMT - . Launch Site: Barents Sea Launch Area. Launch Platform: K-535. LV Family: Topol'. Launch Vehicle: Bulava.
  • RVs - . Nation: Russia. Apogee: 1,000 km (600 mi). Bulava missile test flight from the Yuri Dolgorukiy submarine in the Barents Sea; multiple reentry vehicles flew a suborbital trajectory to the Kura target range in Kamchatka..

2014 November 5

Launch Site: Barents Sea Launch Area. Launch Platform: K-114. LV Family: R-29. Launch Vehicle: Sineva.
  • RV - . Nation: Russia. Apogee: 1,000 km (600 mi). Test flight..

2014 November 28

Launch Site: Barents Sea Launch Area. Launch Platform: K-550. LV Family: Topol'. Launch Vehicle: Bulava.
  • RVs - . Nation: Russia. Apogee: 1,000 km (600 mi). Test flight..

2015 October 30

Launch Site: Barents Sea Launch Area. Launch Platform: K-117. LV Family: R-29. Launch Vehicle: Sineva.
  • R-29RM RV x 4 - . Nation: Russia. Apogee: 1,000 km (600 mi). Test mission. Impacted Kura, Kamchatka..

2015 December 12

Launch Site: Barents Sea Launch Area. Launch Platform: K-51. LV Family: R-29. Launch Vehicle: Sineva.
  • RV x 4? - . Nation: Russia. Apogee: 1,000 km (600 mi). Test mission. Impacted in Kura, Kamchatka..

2016 October 12

Launch Site: Barents Sea Launch Area. Launch Platform: K-407. LV Family: R-29. Launch Vehicle: Sineva.
  • RV - . Nation: Russia. Apogee: 1,000 km (600 mi). Test mission. Impacted in Kura..