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K65M-RB
Part of R-14 Family
Russian orbital launch vehicle. Two stage vehicle for suborbital tests consisting of 1 x R-14 + 1 x S3M.

Status: Retired 1988. First Launch: 1980-12-05. Last Launch: 1988-06-21. Number: 10 . Thrust: 1,485.00 kN (333,841 lbf). Gross mass: 109,000 kg (240,000 lb). Height: 32.40 m (106.20 ft). Diameter: 2.40 m (7.80 ft). Apogee: 250 km (150 mi).


More at: K65M-RB.

Family: orbital launch vehicle. Country: Russia. Spacecraft: BOR-4, BOR-5. Launch Sites: Kapustin Yar, Kapustin Yar LC107/1. Stages: S3, Kosmos-1. Agency: AKO Polyot.

1980 December 5 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. Launch Pad: LC107/pad?. LV Family: R-14. Launch Vehicle: K65M-RB.
  • BOR-4 Re-entry Vehicle test - . Nation: Russia. Agency: RVSN. Apogee: 198 km (123 mi).

1982 June 3 - . 21:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. Launch Pad: LC107/pad?. LV Family: R-14. Launch Vehicle: K65M-RB.
  • Cosmos 1374 - . Mass: 1,000 kg (2,200 lb). Nation: Russia. Agency: MO. Program: Buran. Class: Manned. Type: Manned spaceplane. Spacecraft Bus: Spiral 50-50. Spacecraft: BOR-4. Duration: 0.0700 days. Decay Date: 1982-06-03 . USAF Sat Cat: 13257 . COSPAR: 1982-054A. Apogee: 204 km (126 mi). Perigee: 158 km (98 mi). Inclination: 50.7000 deg. Period: 88.10 min.

    Subscale Spiral spaceplane. After 1.25 revolutions of the earth, deorbited and recovered by Soviet naval forces in the Indian Ocean at 17 degrees South, 98 degrees East, 560 km south of Cocos Islands. Made a 600 km cross-range maneuver during reentry. The recovery was filmed by an Australian Orion reconnaissance aircraft, revealing the configuration to the West for the first time.


1983 March 15 - . 22:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. Launch Pad: LC107/pad?. LV Family: R-14. Launch Vehicle: K65M-RB.
  • Cosmos 1445 - . Mass: 1,000 kg (2,200 lb). Nation: Russia. Agency: MO. Program: Buran. Class: Manned. Type: Manned spaceplane. Spacecraft Bus: Spiral 50-50. Spacecraft: BOR-4. Duration: 0.0700 days. Decay Date: 1983-03-16 . USAF Sat Cat: 13883 . COSPAR: 1983-017A. Apogee: 208 km (129 mi). Perigee: 158 km (98 mi). Inclination: 50.7000 deg. Period: 88.20 min. Subscale Spiral spaceplane. After 1.25 revolutions of the earth, deorbited and recovered by Soviet naval forces in the Indian Ocean, 556 km south of the Cocos Islands ..

1983 December 27 - . 10:00 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. Launch Pad: LC107/pad?. LV Family: R-14. Launch Vehicle: K65M-RB.
  • Cosmos 1517 - . Mass: 1,000 kg (2,200 lb). Nation: Russia. Agency: MO. Program: Buran. Class: Manned. Type: Manned spaceplane. Spacecraft Bus: Spiral 50-50. Spacecraft: BOR-4. Duration: 0.0500 days. Decay Date: 1983-12-27 . USAF Sat Cat: 14585 . COSPAR: 1983-125A. Apogee: 217 km (134 mi). Perigee: 212 km (131 mi). Inclination: 50.7000 deg. Period: 88.80 min. Subscale Spiral spaceplane. In a new mission profile, braked out of orbit over the South Atlantic and was recovered in the Black Sea after one orbit of the Earth..

1984 July 5 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. Launch Pad: LC107/pad?. LV Family: R-14. Launch Vehicle: K65M-RB.
  • BOR-5 sn 501 subscale 1:8 Buran reentry test - . Mass: 1,450 kg (3,190 lb). Nation: Russia. Agency: UNKS. Program: Buran. Spacecraft Bus: Buran. Spacecraft: BOR-5. Apogee: 210 km (130 mi). Range: 2,000 km (1,200 mi). Suborbital test of 1/8 scale model of Buran. Typical trajectory: ascent to 210 km; pitch down to drive model in atmosphere at 45 degree at Mach 18.5. None were reflown but at least 4 were recovered..

1984 December 19 - . 03:55 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. Launch Pad: LC107/pad?. LV Family: R-14. Launch Vehicle: K65M-RB.
  • Cosmos 1614 - . Mass: 1,000 kg (2,200 lb). Nation: Russia. Agency: MO. Program: Buran. Class: Manned. Type: Manned spaceplane. Spacecraft Bus: Spiral 50-50. Spacecraft: BOR-4. Duration: 0.0500 days. Decay Date: 1984-12-19 . USAF Sat Cat: 15442 . COSPAR: 1984-126A. Apogee: 223 km (138 mi). Perigee: 174 km (108 mi). Inclination: 50.7000 deg. Period: 88.50 min. Last flight of the subscale Spiral spaceplane. Recovered December 19, 1984 5:26 GMT, in the Black Sea after one orbit of the Earth..

1985 April 17 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. Launch Pad: LC107/pad?. LV Family: R-14. Launch Vehicle: K65M-RB.
  • BOR-5 sn 502 subscale 1:8 Buran reentry test - . Mass: 1,450 kg (3,190 lb). Nation: Russia. Agency: UNKS. Program: Buran. Spacecraft Bus: Buran. Spacecraft: BOR-5. Apogee: 210 km (130 mi). Range: 2,000 km (1,200 mi). Suborbital test of 1/8 scale model of Buran. Typical trajectory: ascent to 210 km; pitch down to drive model in atmosphere at 45 degree at Mach 18.5. None were reflown but at least 4 were recovered..

1986 December 26 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. Launch Pad: LC107/pad?. LV Family: R-14. Launch Vehicle: K65M-RB.
  • BOR-5 sn 503 subscale 1:8 Buran reentry test - . Mass: 1,450 kg (3,190 lb). Nation: Russia. Agency: UNKS. Program: Buran. Spacecraft Bus: Buran. Spacecraft: BOR-5. Apogee: 210 km (130 mi). Range: 2,000 km (1,200 mi). Suborbital test of 1/8 scale model of Buran. Typical trajectory: ascent to 210 km; pitch down to drive model in atmosphere at 45 degree at Mach 18.5. None were reflown but at least 4 were recovered..

1987 August 27 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. Launch Pad: LC107/pad?. LV Family: R-14. Launch Vehicle: K65M-RB.
  • BOR-5 sn 504 subscale 1:8 Buran reentry test - . Mass: 1,450 kg (3,190 lb). Nation: Russia. Agency: UNKS. Program: Buran. Spacecraft Bus: Buran. Spacecraft: BOR-5. Apogee: 210 km (130 mi). Range: 2,000 km (1,200 mi). Suborbital test of 1/8 scale model of Buran. Typical trajectory: ascent to 210 km; pitch down to drive model in atmosphere at 45 degree at Mach 18.5. None were reflown but at least 4 were recovered..

1988 June 21 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. Launch Pad: LC107/pad?. LV Family: R-14. Launch Vehicle: K65M-RB.
  • BOR-5 sn 505 subscale 1:8 Buran reentry test - . Mass: 1,450 kg (3,190 lb). Nation: Russia. Agency: UNKS. Program: Buran. Spacecraft Bus: Buran. Spacecraft: BOR-5. Apogee: 210 km (130 mi). Range: 2,000 km (1,200 mi). Suborbital test of 1/8 scale model of Buran. Typical trajectory: ascent to 210 km; pitch down to drive model in atmosphere at 45 degree at Mach 18.5. None were reflown but at least 4 were recovered..


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