Encyclopedia Astronautica
VMF


Russian agency. Voenno-Morskoy Flot (Navy), Russia.

More... - Chronology...


Associated People
  • Belyayev Belyayev, Pavel Ivanovich (1925-1970) Russian pilot cosmonaut. Flew on Voskhod 2. More...
  • Rozhdestvensky Rozhdestvensky, Valeri Illyich (1939-) Russian engineer cosmonaut. Flew on Soyuz 23. More...

Associated Countries
See also
  • Agency Agencies or institutions overseeing design, development, construction, or operation of space-related systems. More...

Associated Programs
  • EORSAT Naval forces monitoring. Determines position of enemy naval forces through detection and triangulation of their electromagnetic emissions (radio, radar, etc) More...

Associated Launch Sites
  • Nenoksa Primary missile testing range of the Russian Navy. Known to have been used for 22 launches from 1965 to 1997, reaching up to 1000 kilometers altitude, but the number of actual missile tests was in the hundreds. More...

VMF Chronology


1959 - . Launch Site: Sea-launched. Launch Pad: BELA. Launch Platform: B-67. LV Family: R-11. Launch Vehicle: R-11FM. FAILURE: Failure.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 0 km ( mi).

1960 September 10 - . Launch Site: Sea-launched. Launch Pad: BELA. Launch Platform: B-67. LV Family: R-11. Launch Vehicle: R-11FM.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 200 km (120 mi).

1969 March 1 - . Launch Site: Nenoksa. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1969 June 21 - . Launch Site: Nenoksa. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1970 - . Launch Site: Nenoksa. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1971 - . Launch Site: Nenoksa. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1971 December 15 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1972 Jan - . Launch Site: White Sea Launch Area. Launch Vehicle: Vysota. LV Configuration: Vysota R-29.
  • - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1972 Mar - . Launch Site: White Sea Launch Area. Launch Vehicle: Vysota. LV Configuration: Vysota R-29.
  • - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1972 Apr - . Launch Site: White Sea Launch Area. Launch Vehicle: Vysota. LV Configuration: Vysota R-29.
  • - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1972 May - . Launch Site: White Sea Launch Area. Launch Vehicle: Vysota. LV Configuration: Vysota R-29.
  • - . Nation: USSR. Agency: VMF. Apogee: 0 km ( mi).

1972 August 1 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E..

1972 September 1 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E..

1972 October 1 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E..

1972 November 25 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E..

1972 November 28 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E..

1972 November 28 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E..

1972 December 14 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E..

1972 December 14 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E..

1972 December 14 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E..

1972 December 14 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E..

1974 February 1 - . Launch Site: Nenoksa. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1974 February 1 - . Launch Site: Nenoksa. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1974 September 1 - . Launch Site: Nenoksa. LV Family: R-29. Launch Vehicle: Vysota.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1974 Oct - . Launch Site: White Sea Launch Area. Launch Vehicle: Vysota.
  • - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1974 Oct - . Launch Site: White Sea Launch Area. Launch Vehicle: Vysota.
  • - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1975 - . Launch Site: Nenoksa. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1976 - . Launch Site: Nenoksa. LV Family: R-29. Launch Vehicle: Vysota.
  • Operational test - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1976 November 1 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E..

1977 Q1 - . Launch Site: Sea-launched. Launch Pad: UNKPL. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 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: USSR. 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: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1977 November 1 - . Launch Site: Sea-launched. Launch Pad: UNKPL. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1977 November 1 - . Launch Site: Sea-launched. Launch Pad: UNKPL. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1977 November 1 - . Launch Site: Sea-launched. Launch Pad: UNKPL. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1977 December 1 - . Launch Site: Sea-launched. Launch Pad: UNKPL. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1978 September 1 - . Launch Site: Sea-launched. Launch Pad: UNKPL. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1980 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF.
  • Test mission - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Launched from White Sea Launch Area, Beloye More, Archangel'sk Oblast' - Latitude: 65.50 N - Longitude: 38.00 E..

1981 - . Launch Site: Okhotsk. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF.
  • Operational test - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1981 - . Launch Site: Okhotsk. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Operational test - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1981 - . Launch Site: Okhotsk. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Operational test - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1981 - . Launch Site: Okhotsk. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF.
  • Operational test - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1981 - . Launch Site: Okhotsk. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF.
  • Operational test - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1981 - . Launch Site: Okhotsk. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Operational test - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1981 - . Launch Site: Okhotsk. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Operational test - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1983 June 1 - . Launch Site: Nenoksa. LV Family: R-29. Launch Vehicle: Shtil. LV Configuration: Shtil VMF.
  • State trials missile test - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1984 September 7 - . 07:10 GMT - . Launch Site: Barents Sea Launch Area. Launch Vehicle: Volna. LV Configuration: Volna VMF.
  • Caused UFO sighting - . Nation: USSR. 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: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1991 December 1 - . Launch Site: Sea-launched. Launch Pad: UNKPL. Launch Platform: KALMAR. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF.
  • Operational test - . Nation: USSR. Agency: VMF. Apogee: 1,000 km (600 mi).

1992 - . Launch Site: Sea-launched. Launch Pad: UNKPL. Launch Platform: KALMAR. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF RF.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1993 December 1 - . Launch Site: Sea-launched. Launch Pad: UNKPL. Launch Platform: KALMAR. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF RF.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 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 SLV. LV Configuration: Volna VMF RF.
  • Volan? - . Nation: Russia. Agency: VMF. Apogee: 1,270 km (780 mi).

1995 August 25 - . Launch Site: Arctic Ocean. Launch Pad: 90.0 N x 0.0 E. Launch Platform: TK-20. LV Family: R-39. Launch Vehicle: Rif.
  • Test mission - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1996 - . Launch Site: Nenoksa. LV Family: R-39. Launch Vehicle: Grom. FAILURE: Failure.
  • Test mission - . Nation: Russia. Agency: RVSN; VMF. Apogee: 0 km ( mi).

1996 June 28 - . Launch Site: Okhotsk. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1996 June 28 - . Launch Site: Okhotsk. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Vysota.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1996 June 28 - . Launch Site: Okhotsk. Launch Platform: PLBR. 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 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 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? - . Launch Site: Nenoksa. LV Family: R-39. Launch Vehicle: Grom. FAILURE: Failure.
  • Test mission - . Nation: Russia. Agency: RVSN; VMF. Apogee: 0 km ( 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 SLV.
  • 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 July 23 - . Launch Site: Okhotsk. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Volna SLV.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 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 ( 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 - . 03:15 GMT - . 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-1/1N.
  • 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: 78.9000 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: 78.9000 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 SLV.
  • 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 SLV.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1999 October 1 - . Launch Site: Okhotsk. Launch Platform: K-211. LV Family: R-29. Launch Vehicle: Volna SLV.
  • 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 SLV. FAILURE: Failure.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

1999 October 2 - . Launch Site: Okhotsk. Launch Platform: K-211. LV Family: R-29. Launch Vehicle: Volna SLV.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

1999 December 26 - . 08:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/20. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2. LV Configuration: Tsiklon-2 801 (45082801).
  • Cosmos 2367 - . Payload: US-PM s/n 10. Mass: 3,150 kg (6,940 lb). Nation: Russia. Agency: VMF. Manufacturer: Arsenal. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: US-PU. Decay Date: 2002-07-19 . USAF Sat Cat: 26040 . COSPAR: 1999-072A. Apogee: 418 km (259 mi). Perigee: 404 km (251 mi). Inclination: 65.0000 deg. Passive naval electronic intelligence satellite. The satellite was placed in an initial 147 km x 442 km orbit at 65 degree inclination. The US-PM's propulsion module fired at apogee to circularize the orbit. Replaced the only previous remaining US-PM satellite which ended operations in November and reentered earlier in December 1999.

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). Summary: 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: Shtil.
  • 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. LV Configuration: Shtil VMF RF.
  • 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. LV Configuration: Shtil VMF RF.
  • 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. LV Configuration: Shtil VMF RF.
  • 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 SLV.
  • 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 18 - . Launch Site: Okhotsk. Launch Platform: PODOLSK. LV Family: R-29. Launch Vehicle: Shtil. LV Configuration: Shtil VMF RF.
  • 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. LV Configuration: Shtil VMF RF.
  • 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. LV Configuration: Shtil VMF RF.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2001 October 18 - . 09:00 GMT - . Launch Site: Sea-launched. Launch Pad: BELA. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Shtil. LV Configuration: Shtil VMF RF.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Launched from a Russian submarine in the White Sea Launch Area off Arkhangelsk - Latitude: 65.5 N, Longitude:38 E..

2001 December 21 - . 04:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/20. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2.
  • Cosmos 2383 - . Payload: US-PM s/n 11. Mass: 3,150 kg (6,940 lb). Nation: Russia. Agency: VMF. Manufacturer: Arsenal. Program: EORSAT. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: US-PU. Decay Date: 2004-03-20 . USAF Sat Cat: 27053 . COSPAR: 2001-057A. Apogee: 415 km (257 mi). Perigee: 404 km (251 mi). Inclination: 65.0000 deg. Signal Intelligence Satellite. Launch delayed December 19. The booster put the satellite into an initial orbit of 145 x 405 km x 65.0 deg. At apogee the satellite ignited its own propulsion system to increase velocity by about 70-80 m/s and circularize the orbit.

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 SLV.
  • 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 - . 09:12 GMT - . Launch Site: Okhotsk. Launch Platform: PLBR. LV Family: R-29. Launch Vehicle: Shtil. LV Configuration: Shtil VMF RF.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

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. LV Configuration: Shtil VMF RF.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2003 October 15 - . 10:03 GMT - . Launch Site: Sea-launched. Launch Pad: BLA. LV Family: R-29. Launch Vehicle: R-29RM. LV Configuration: R-29RM.
  • RSM-54 test launch - . Nation: Russia. Agency: VMF.

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. LV Configuration: Sineva VMF RF. FAILURE: Failure.
  • Sineva operational test - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi). Summary: 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. LV Configuration: Sineva VMF RF.
  • 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. LV Configuration: Sineva VMF RF.
  • Operational test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2004 May 28 - . 06:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/20. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2.
  • Cosmos 2405 - . Mass: 3,150 kg (6,940 lb). Nation: Russia. Agency: VMF. Manufacturer: Arsenal. Program: EORSAT. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: US-PU. Decay Date: 2006-06-16 . USAF Sat Cat: 28350 . COSPAR: 2004-020A. Apogee: 417 km (259 mi). Perigee: 405 km (251 mi). Inclination: 65.0000 deg. Period: 92.80 min. Summary: Original reported name Cosmos 2407..

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 SLV.
  • - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: 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. Launch Vehicle: Bulava.
  • Bulava cold-launch test - . Nation: Russia. Agency: VMF. Apogee: 1.00 km (0.60 mi). Summary: 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 November 2 - . 09:25 GMT - . Launch Site: Okhotsk. Launch Platform: K-433. LV Family: R-29. Launch Vehicle: Volna SLV.
  • RSM-54 test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2004 December 11 - . Launch Site: Barents Sea Launch Area. Launch Pad: 69.5 N x 34.2 E. Launch Platform: TK-208. Launch Vehicle: Bulava.
  • Bulava cold-launch test - . Nation: Russia. Agency: VMF. Apogee: 1.00 km (0.60 mi). Summary: A mass replica of a the new Bulava SLBM was ejected from its launch tube from the surfaced SSBN Dmitry Donskoi..

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. LV Configuration: Sineva VMF RF.
  • RSM-54 test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2005 September 30 - . 08:22 GMT - . Launch Site: Okhotsk. Launch Platform: K-433. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF RF.
  • RSM-50 Test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Search for payload at reentry site was unsuccessful. Delayed from fourth quarter 2003, May and October 2004, July 5/8, September 15 and 27, 2005..

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 SLV.
  • 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. LV Configuration: Sineva VMF RF.
  • RSM-54 Test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2006 June 24 - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/20. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2.
  • Cosmos 2421 - . Mass: 3,150 kg (6,940 lb). Nation: Russia. Agency: VMF. Manufacturer: Arsenal. Program: EORSAT. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: US-PU. Decay Date: 2006-06-24 . USAF Sat Cat: 29246 . COSPAR: 2006-026A. Apogee: 414 km (257 mi). Perigee: 384 km (238 mi). Inclination: 65.0000 deg. Period: 92.50 min.

2006 June 30 - . 06:25 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: Sineva. LV Configuration: Sineva VMF RF.
  • R-29RM test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2006 September 7 - . 15:50 GMT - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: TK-208. Launch Vehicle: Bulava. FAILURE: Failure.
  • Bulava SLBM test - . Nation: Russia. Agency: VMF. Apogee: 1.00 km (0.60 mi).

2006 September 9 - . 11:20 GMT - . Launch Site: Arctic Ocean. Launch Pad: 90.0 N x 0.0 E. Launch Platform: K-84. LV Family: R-29. Launch Vehicle: Sineva. LV Configuration: Sineva VMF RF.
  • R-29RM test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). Submarine K-84 Ekaterinburg launched the missile while surfaced in the ice pack from a polar location toward the Chizha impact zone on the Kanin Peninsula. The three warheads were reported to have successfuly reached their targets. This was the first Russian launch from the icepack since 29 August 1995.

2006 September 10 - . 14:50 GMT - . Launch Site: Pacific Ocean. Launch Pad: 47.0 N x 152.0 E. Launch Platform: K-433. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF RF.
  • R-29R test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Submarine K-433 St Georgiy Pobedonosets launched the missile from the Pacific near Simushir Island towards an impact zone on the Kanin Peninsula. The two warheads were reported to have successfully reached their targets..

2006 October 25 - . 13:05 GMT - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: TK-208. Launch Vehicle: Bulava. FAILURE: Failure.
  • Bulava SLBM test - . Nation: Russia. Agency: VMF. Apogee: 100 km (60 mi).

2006 December 24 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: TK-208. Launch Vehicle: Bulava. FAILURE: Failure.
  • - . Nation: Russia. Agency: VMF. Apogee: 1.00 km (0.60 mi).

2007 June 28 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: TK-208. LV Family: Bulava. Launch Vehicle: Bulava.
  • Bulava SLBM test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: The warhead impacted on target in the Kamchatka Peninsula. This was the first successful launch after two consecutive failures..

2007 August 7 - . Launch Site: Sea-launched. Launch Pad: POR. Launch Platform: K-211. LV Family: R-29. Launch Vehicle: Volna SLV. LV Configuration: Volna VMF RF.
  • 1 RV SLBM test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2007 November 10 - . Launch Site: White Sea Launch Area. Launch Pad: 65.5 N x 38.0 E. Launch Platform: TK-208. LV Family: Bulava. Launch Vehicle: Bulava. FAILURE: Failure.
  • R&D - . Nation: Russia. Agency: VMF. Apogee: 1.00 km (0.60 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: Sineva. LV Configuration: Sineva VMF RF.
  • - . 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. LV Configuration: Sineva VMF RF.
  • - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2008 September 18 - . 14:45 GMT - . Launch Site: White Sea Launch Area. LV Family: Bulava. Launch Vehicle: Bulava. LV Configuration: Bulava R-30 08.
  • Kura - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi).

2008 November 28 - . Launch Site: Barents Sea. Launch Platform: TK-208. LV Family: Bulava. Launch Vehicle: Bulava.
2008 December 23 - . 03:00 GMT - . Launch Site: Barents Sea. Launch Platform: TK-208. LV Family: Bulava. Launch Vehicle: Bulava.
  • RV-1 - . Nation: Russia. Agency: VMF. Class: Technology. Type: Technology satellite. Apogee: 100 km (60 mi).

2009 July 13 - . Launch Site: North Pole. Launch Platform: K-177. LV Family: R-29. Launch Vehicle: Sineva.
  • Sineva Test - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Test.

2009 July 15 - . Launch Site: White Sea Launch Area. LV Family: Bulava. Launch Vehicle: Bulava. LV Configuration: Bulava R-30 11 3M30.
  • St 1 fail (Kura) - . Nation: Russia. Agency: VMF. Apogee: 10 km (6 mi).

2009 October 6 - . Launch Site: Okhotsk. Launch Platform: K-43. LV Family: R-29. Launch Vehicle: Volna SLV.
  • Volna RV - . Mass: 1,000 kg (2,200 lb). Nation: Russia. Agency: VMF. Summary: Operational test.

2009 October 7 - . Launch Site: Okhotsk. Launch Platform: K-44. LV Family: R-29. Launch Vehicle: Volna SLV.
  • Volna RV - . Mass: 1,000 kg (2,200 lb). Nation: Russia. Agency: VMF. Summary: Operational test.

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. Summary: Operational test.

2009 December 9 - . 06:45 GMT - . Launch Site: White Sea Launch Area. Launch Platform: TK-208. LV Family: Bulava. Launch Vehicle: Bulava.
  • Bulava test - . Nation: Russia. Agency: VMF. Summary: Failed Bulava launch. Third stage went into a wild spiral maneuver, creating a tremendous celestial spectacle visible all over Scandinavia..

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). Summary: Operational test launch.

2010 August 6 - . 15:15 GMT - . Launch Site: Barents Sea Launch Area. Launch Platform: Tula. LV Family: R-29. Launch Vehicle: Sineva.
  • RV x4 - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Operational test..

2010 August 6 - . 15:15 GMT - . Launch Site: Barents Sea Launch Area. Launch Platform: Tula. LV Family: R-29. Launch Vehicle: Sineva.
  • RV x4 - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: Operational test..

2010 October 7 - . 03:10 GMT - . Launch Site: White Sea Launch Area. Launch Platform: TK-208. LV Family: Bulava. Launch Vehicle: Bulava.
  • RV x 3 - . Nation: Russia. Agency: VMF. Apogee: 1,000 km (600 mi). Summary: R&D test..

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