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K65M-RB

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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).

• BOR-4 Re-entry Vehicle test - . Nation: Russia. Agency: RVSN. Apogee: 198 km (123 mi).

• 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: 50.70 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.

• 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: 50.70 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 ..

• 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: 50.70 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..

• 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..

• 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: 50.70 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..

• 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..

• 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..

• 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..

• 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..