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Baikonur LC1
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Area 1 - Launch Site: Baikonur. Launch Pads: 1. Latitude: 45.9120 N. Longitude: 63.3500 E. Luna 8K72, Molniya 8K78, Molniya 8K78M, R-7, R-7A, Soyuz 11A511, Soyuz 11A511U, Soyuz 11A511U2, Soyuz FG, Voskhod 11A57, Vostok 8A92, Vostok 8K72, Vostok 8K72K. - 1957 May 15 16:01 - M1-5 (I-1) Test mission Launch Vehicle: R-7. Failure of Block D strapon, which tore away from the core 98 seconds after liftoff. The booster crashed 400 km from the pad. A fuel leak in the pump outlet led to a fire in the engine compartment from the time of liftoff.. R-7 No. 5L Apogee: 1.00 km (0.60 mi). R-7 test flight. (M1-5 (I-1))
- 1957 July 12 12:53 - M1-7 (I-2) Test mission Launch Vehicle: R-7. Failure of the control system due to a short circuit of the battery. Rapid roll developed, resulting in all four strap-on boosters flying away from the core at 33 seconds in the flight.. R-7 No. 7 R-7 test flight. (M1-7 (I-2))
- 1957 August 21 12:25 - M1-9 (I-3) Test mission Launch Vehicle: R-7. R-7 No. 8 Apogee: 1,000 km (600 mi). First successful ICBM flight. Problems with the curing of the nose cone material, known before launch, led to the dummy warhead disintegrating over the Kamchatka Peninsula.
- 1957 September 7 11:39 - M1-10 (I-4) Test mission Launch Vehicle: R-7. R-7 No. 9 Apogee: 1,000 km (600 mi). Second successful ICBM flight.
- 1957 October 4 19:28 - Sputnik 1 Launch Vehicle: R-7. Sputnik 8K71PS No. 1PS Apogee: 945 km (587 mi). First artificial satellite; transmitted signals for 21 days. Launching of first ever artificial satellite of the Earth; physical study of the atmosphere; remained in orbit until January 4, 1958. This event began the space race by galvanizing interest and action on the part of the American public to support an active role in space research, technology, and exploration.
- 1957 November 3 02:30 - Sputnik 2 Launch Vehicle: R-7. Sputnik 8K71PS No. 2PS Apogee: 1,660 km (1,030 mi). Carried dog Laika. Study of the physical processes and conditions of life in outer space. After the surprise public impact of Sputnik 1, the satellite and launch teams were called back from vacation and in one month assembled the satellite (using equipment already developed for dog sounding rocket flights). After the launch, Soviet space officials said that the spacecraft would not return and that the dog had enough food and oxygen to live for up to 10 days. Only 45 years later was it revealed that Laika overheated, panicked and died within 5 to 7 hours of launch. What turned out to be the first space crypt remained in orbit a total of 162 days, then burned up in the atmosphere on April 14, 1958.
- 1958 January 29 21:15 - M1-12 (I-5) Test mission Launch Vehicle: R-7. The missile exploded a few seconds after liftoff.. R-7 No. 11 Apogee: 1,000 km (600 mi). Last test of the original R-7 8K71 test series. Suborbital launch test.
- 1958 March 29 14:40 - M1-6A (I-6) Test mission Launch Vehicle: R-7. R-7 No. 10 Apogee: 1,000 km (600 mi). R-7 test flight. (M1-6A (I-6))
- 1958 April 4 15:30 - B1-11 (I-7) Test mission Launch Vehicle: R-7. R-7 No. 12 Apogee: 1,000 km (600 mi). R-7 test flight. (B1-11 (I-7))
- 1958 April 27 - Sputnik failure Launch Vehicle: R-7. Launch vehicle disintegrated 88 seconds after liftoff.. Sputnik 8A91 B1-2
- 1958 May 15 07:00 - Sputnik 3 Launch Vehicle: R-7. Sputnik 8A91 B1-1 Apogee: 1,864 km (1,158 mi). Variety of scientific data. Research in the upper atmosphere and outer space
- 1958 May 24 10:30 - B1-3 (II-1) Test mission Launch Vehicle: R-7. Failure. R-7 No. 3 Apogee: 1,000 km (600 mi). R-7 test flight. (B1-3 (II-1))
- 1958 July 10 07:42 - B1-4 (II-2)/Blok E Test mission Launch Vehicle: R-7. Failure. R-7 71/III No. 6
- 1958 September 23 - Luna failure - booster disintegrated at T+92 seconds Launch Vehicle: Luna 8K72. Launcher disintegrated 93 seconds after launch due to longitudinal resonance of strap-ons.. Vostok-L 8K72 B1-3 This was the start of an acrimonious debated between Glushko and Korolev design bureaux over the fault and fix for the problem.
- 1958 October 11 08:42 - Luna failure - booster disintegrated at T+104 seconds Launch Vehicle: Luna 8K72. Launcher disintegrated 104 seconds after launch due to longitudinal resonance of strap-ons.. Vostok-L 8K72 B1-4
- 1958 December 4 - Luna failure - booster core shut down at T+245 seconds Launch Vehicle: Luna 8K72. Core engines shut off at 245 seconds into the flight. Cause was a loss of lubrication to the hydrogen peroxide pump.. Vostok-L 8K72 B1-5
- 1958 December 24 16:00 - III-1 Test mission Launch Vehicle: R-7. Failure..
- 1959 January 2 16:41 - Luna 1 Launch Vehicle: Luna 8K72. Failure of the launch vehicle control system.. Vostok-L 8K72 B1-6 Lunar probe; passed within 5,995 km of moon but did not hit it as planned due to a failure of the launch vehicle control system. Went into solar orbit. First manmade object to attain of escape velocity. Also known as Mechta ("Dream"), popularly called Lunik I. Because of its high velocity and its announced package of various metallic emblems with the Soviet coat of arms, it was concluded that Luna 1 was intended to impact the Moon. After reaching escape velocity, Luna 1 separated from its 1472 kg third stage. The third stage, 5.2 m long and 2.4 m in diameter, travelled along with Luna 1. On 3 January, at a distance of 113,000 km from Earth, a large (1 kg) cloud of sodium gas was released by the spacecraft. This glowing orange trail of gas, visible over the Indian Ocean with the brightness of a sixth-magnitude star, allowed astronomers to track the spacecraft. It also served as an experiment on the behavior of gas in outer space. Luna 1 passed within 5,995 km of the Moon's surface on 4 January after 34 hours of flight. It went into orbit around the Sun, between the orbits of Earth and Mars. The measurements obtained during this mission provided new data on the Earth's radiation belt and outer space, including the discovery that the Moon had no magnetic field and that a solar wind, a strong flow of ionized plasma emmanating from the Sun, streamed through interplanetary space.
- 1959 March 17 01:46 - GCh No. 13 (III-2) Test mission Launch Vehicle: R-7. R-7 No. 81 Apogee: 1,000 km (600 mi). First test flight serial production model.
- 1959 March 25 05:25 - GCh No. 15 (III-3) Test mission Launch Vehicle: R-7. R-7 No. 18 Apogee: 1,000 km (600 mi). R-7 development test flight. (GCh No. 15 (III-3))
- 1959 March 30 22:53 - GCh No. IZ-20 (III) Test mission Launch Vehicle: R-7. Failure..
- 1959 May 9 18:59 - GCh No. 17 (III) Test mission Launch Vehicle: R-7. Failure. R-7 No. 21 R-7 development test flight. (GCh No. 17 (III))
- 1959 May 30 21:42 - GCh No. IZ-22 (III) Test mission Launch Vehicle: R-7. Failure. Landed far from aim point.
- 1959 June 9 20:34 - GCh No. IZ-23 (III) Test mission Launch Vehicle: R-7. Failure. Landed far from aim point.
- 1959 June 18 - Luna failure - inertial system failed at T+153 seconds Launch Vehicle: Luna 8K72. Inertial system failed at 153 seconds after launch. Vehicle destroyed by range safety.. Vostok-L 8K72 I1-7
- 1959 July 18 18:15 - GCh No. IZ-24 (III) Test mission Launch Vehicle: R-7. R-7 No. 24 Apogee: 1,000 km (600 mi). R-7 development test flight. (GCh No. IZ-24 (III))
- 1959 July 30 04:00 - GCh (III) Test mission Launch Vehicle: R-7. R-7 No. 041082 Apogee: 1,000 km (600 mi). First successful flight of series production model.
- 1959 August 13 23:14 - GCh No. IZ-25 (III) Test mission Launch Vehicle: R-7. Apogee: 1,000 km (600 mi).
- 1959 September 12 06:39 - Luna 2 Launch Vehicle: Luna 8K72. Vostok-L 8K72 I1-7B First probe to impact lunar surface. Delivered a pennant to the surface of the Moon and conducted research during flight to the Moon. Impacted Moon 13 Sep 1959 at 22:02:04 UT, Latitude 29.10 N, Longitude 0.00 - Palus Putredinis, east of Mare Serenitatis near the Aristides, Archimedes, and Autolycus craters. After launch and attainment of escape velocity, Luna 2 separated from its third stage, which travelled along with it towards the Moon. On 13 September the spacecraft released a bright orange cloud of sodium gas which aided in spacecraft tracking and acted as an experiment on the behavior of gas in space. On 14 September, after 33.5 hours of flight, radio signals from Luna 2 abruptly ceased, indicating it had impacted on the Moon. Some 30 minutes after Luna 2, the third stage of its rocket also impacted the Moon. The mission confirmed that the Moon had no appreciable magnetic field, and found no evidence of radiation belts at the Moon.
- 1959 September 18 16:02 - Phase 3 test flight Launch Vehicle: R-7. R-7 I1-1T Apogee: 1,000 km (600 mi). R-7 development test flight.
- 1959 October 4 00:43 - Luna 3 Launch Vehicle: Luna 8K72. Vostok-L 8K72 I1-8 Luna 3 was the third spacecraft successfully launched to the Moon and the first to return images of the lunar far side. It was launched on a figure-eight trajectory which brought it over the Moon (closest approach to the Moon was 6200 km) and around the far side, which was sunlit at the time. It was stabilized while in optical view of the far side of the Moon. On October 7, 1959, the television system obtained a series of 29 photographs over 40 minutes, covering 70% of the surface, that were developed on-board the spacecraft. The photographs were scanned and 17 were radio transmitted to ground stations in facsimile form on October 18, 1959, as the spacecraft, in a barycentric orbit, returned near the Earth. The photographs were to be retransmitted at another point close to Earth but were not received. The spacecraft returned very indistinct pictures, but, through computer enhancement, a tentative atlas of the lunar farside was produced. These first views of the lunar far side showed mountainous terrain, very different from the near side, and two dark regions which were named Mare Moscovrae (Sea of Moscow) and Mare Desiderii (Sea of Dreams).
- 1959 October 22 17:30 - Phase 3 test flight Launch Vehicle: R-7. Apogee: 1,000 km (600 mi).
- 1959 October 25 17:32 - Phase 3 test flight Launch Vehicle: R-7. Apogee: 1,000 km (600 mi).
- 1959 November 1 21:23 - Phase 3 test flight Launch Vehicle: R-7. R-7 No. 267431 Apogee: 1,000 km (600 mi). Flight over full missile design range.
- 1959 November 20 21:06 - Phase 3 test flight Launch Vehicle: R-7. R-7 I2-1T Apogee: 1,000 km (600 mi). Flight over full missile design range.
- 1959 November 27 01:12 - GCh No. IZ-33 (III) Test mission Launch Vehicle: R-7. Apogee: 1,000 km (600 mi). Sixteenth and last launch of the third production batch.
- 1959 December 23 19:05 - R-7A I-1 Test mission Launch Vehicle: R-7A. Failed due to engine steering not engaging.. R-7A I1-1 Apogee: 1,000 km (600 mi).
- 1960 Jan 20 1635? 16:35 - R-7A I-2/Dummy L Test mission Launch Vehicle: Molniya 8K78. Molniya 8K78 I1-2 Apogee: 200 km (120 mi). Suborbital aerodynamic test flight with R-7A 8K74 lower stages, dummy upper stages.
- 1960 January 24 16:15 - R-7A I-3 Test mission Launch Vehicle: R-7A. Failure.. R-7A I1-3
- 1960 Jan 31 0530? 05:30 - R-7A I-4/Dummy L Test mission Launch Vehicle: Molniya 8K78. Molniya 8K78 I1-4 Apogee: 200 km (120 mi). Suborbital aerodynamic test flight with R-7A 8K74 lower stages, dummy upper stages.
- 1960 March 17 23:55 - R-7A I-4 Test mission Launch Vehicle: R-7A. R-7A L1-5 Apogee: 1,000 km (600 mi).
- 1960 March 24 02:06 - R-7A I-5 Test mission Launch Vehicle: R-7A. Apogee: 1,000 km (600 mi).
- 1960 April 15 - Luna failure - third stage insufficient delta V Launch Vehicle: Luna 8K72. The third stage RO-5 engine either did not reach full thrust or shut down early.. Vostok-L 8K72 L1-9 Reached an altitude of 200,000 km before plunging back to earth.
- 1960 April 16 16:07 - Luna failure at lift-off Launch Vehicle: Luna 8K72. Strap-on B reached only 75 percent of thrust at ignition. Four tenths of a second after liftoff it broke away from the core.. Vostok-L 8K72 L1-9A This dramatic failure resulted in a loss of thrust, and the lateral strap-on units separated and flew over the tracking stations and living areas. The core continued on its trajectory.
- 1960 May 15 - Korabl-Sputnik 1 Launch Vehicle: Vostok 8K72. Vostok 8K72 L1-11 Apogee: 514 km (319 mi). The Soviet Union launched a Vostok 1KP prototype manned spacecraft (without heat shield; not recoverable) into near-earth orbit. Called Sputnik IV by the Western press. On May 19, at 15:52 Moscow time, the spacecraft was commanded to retrofire. However the guidance system had oriented the spacecraft incorrectly and the TDU engine instead put the spacecraft into a higher orbit. Soviet scientists said that conditions in the cabin, which had separated from the remainder of the spacecraft, were normal.
Officially: Development and checking of the main systems of the space ship satellite, which ensure its safe flight and control in flight, return to Earth and conditions needed for a man in flight.
- 1960 June 4 15:49 - UBP (Readiness) operational test launch Launch Vehicle: R-7. R-7 L1-9 Apogee: 1,000 km (600 mi). R-7 readiness verification test.
- 1960 July 5 15:56 - R-7A I-6 Test mission Launch Vehicle: R-7A. Apogee: 1,000 km (600 mi).
- 1960 July 7 15:27 - R-7A I-7 Test mission Launch Vehicle: R-7A. Apogee: 1,000 km (600 mi).
- 1960 July 28 - Korabl-Sputnik Launch Vehicle: Vostok 8K72. At ignition one of the combustion chambers in strapon Block B or G burned through. The strapon separated from the core at 17 seconds into the flight and the launch vehicle exploded at 28.5 seconds.. Vostok 8K72 L1-10 First attempted flight of the Vostok 1K manned spacecraft prototype. Dogs Chaika and Lisichka perished in the explosion of the rocket.
- 1960 August 19 08:44 - Korabl-Sputnik 2 Launch Vehicle: Vostok 8K72. Vostok 8K72 L1-12 Apogee: 340 km (210 mi). The Soviet Union launched its second unmanned test of the Vostok spacecraft, the Korabl Sputnik II, or Sputnik V. The spacecraft carried two dogs, Strelka and Belka, in addition to a gray rabbit, rats, mice, flies, plants, fungi, microscopic water plants, and seeds. Electrodes attached to the dogs and linked with the spacecraft communications system, which included a television camera, enabled Soviet scientists to check the animals' hearts, blood pressure, breathing, and actions during the trip. After the spacecraft reentered and landed safely the next day, the animals and biological specimens were reported to be in good condition.
Officially: Development of systems ensuring man's life functions and safety in flight and his return to Earth.
- 1960 October 10 14:27 - Mars probe 1M s/n 1 failure. Launch Vehicle: Molniya 8K78. At T+300.9 sec, the launcher went out of control and the destruct command was given at T+324.2 sec - the engine of Stage 3 cut off after 13.32 s of burning.. Molniya 8K78 L1-4M This was the Soviet Union's first attempt at a planetary probe. Mars probe intended to photograph Mars on a flyby trajectory. The possible cause lay in resonance vibrations of upper stages during Stage 2 burning, which led to break of contact in the command potentiometer of the gyrohorizon. As a result a pitch control malfunctioned and the launcher began to veer off the desired ascent profile. On exceeding 7 degrees of veering in pitch, the control system failed. The upper stage with the payload reached an altitude of 120 km before burning up on re-entry into the atmosphere above East Siberia.
- 1960 October 14 13:51 - Mars probe 1M s/n 2 failure. Launch Vehicle: Molniya 8K78. At T+290 sec Stage 3's engine 8D715K failed to ignite because a LOX leak froze kerosene in the fuel inlet to the pump on the launch pad due to a faulty LOX valve seal.. Molniya 8K78 L1-5M Mars probe intended to photograph Mars on a flyby trajectory. This was the Soviet Union's second attempt at a planetary probe. The upper stages and payload broke up on re-entry into the atmosphere.
- 1960 December 1 07:30 - Korabl-Sputnik 3 Launch Vehicle: Vostok 8K72. Vostok 8K72 L1-13 Apogee: 269 km (167 mi). The Soviet Union launched its third spaceship satellite, Korabl Sputnik III, or Sputnik VI. The spacecraft, similar to those launched on May 15 and August 19, carried the dogs Pcheka and Mushka in addition to other animals, insects, and plants. Deorbited December 2, 1960 7:15 GMT. Burned up on reentry due to steep entry angle (retrofire engine did not shut off on schedule and burned to fuel depletion).
Officially: Medical and biological research under space flight conditions.
Officially: Medical and biological research under space flight conditions.
- 1960 December 22 - Korabl-Sputnik Launch Vehicle: Vostok 8K72K. The third stage engine RO-7 failed just after ignifition, 425 seconds in to flight.. Vostok 8K72K L1-13A Unable to reach orbital velocity, the Vostok prototype separated while the third stage was still firing. While the ejection seat failed to operate, the capsule did make a hard landing in severe winter conditons in Siberia. It was recovered after some time, and the dogs Kometa and Shutka were alive. As a result of this flight the ejection seat was developed with a heat shield designed to protect the pilot in the event of a launch vehicle failure up to shut down of the first stage.
- 1961 - Operational Test mission Launch Vehicle: R-7A. Apogee: 1,000 km (600 mi).
- 1961 February 4 01:18 - Sputnik 7 Launch Vehicle: Molniya 8K78. At T+531 sec, the fourth vernier chamber of Stage 3's 8D715K engine exploded because the LOX cut-off valve had not closed as scheduled and LOX flowed into the hot chamber.. Molniya 8K78 L1-7 Apogee: 318 km (197 mi). The escape stage entered parking orbit but the main engine cut off just 0.8 s after ignition due to cavitation in the oxidiser pump and pump failure.. The payload attached together with escape stage remained in Earth orbit.
The booster launched into a beautiful clear sky, and it could be followed by the naked eye for four minutes after launch. The third stage reached earth parking orbit, but the fourth stage didn't ignite. It was at first believed a radio antenna did not deploy from the interior of the stage, and it did not receive the ignition commands. Therefore the Soviet Union has successfully orbited a record eight-tonne 'Big Zero' into orbit. The State Commission meets two hours after the launch, and argues whether to make the launch public or not, and how to announce it. Glushko proposes the following language for a public announcement: 'with the objective of developing larger spacecraft, a payload was successfully orbited which provided on the first revolution the necessary telemetry'. Korolev and the others want to minimize any statement, to prevent speculation that it was a reconnaissance satellite or a failed manned launch. Kamanin's conclusion - the rocket didn't reach Venus, but it did demonstrated a new rocket that could deliver an 8 tonne thermonuclear warhead anywhere on the planet. The commission heads back to Moscow.
- 1961 February 12 00:34 - Venera 1 Launch Vehicle: Molniya 8K78. Molniya 8K78 L1-6B Venera 1 was the first spacecraft to fly by Venus. The 6424 kg assembly was launched first into a 229 x 282 km parking orbit, then boosted toward Venus by the restartable Molniya upper stage. On 19 February, 7 days after launch, at a distance of about two million km from Earth, contact with the spacecraft was lost. On May 19 and 20, 1961, Venera 1 passed within 100,000 km of Venus and entered a heliocentric orbit. This failure resulted in only the following objectives being met: checking of methods of setting space objects on an interplanetary course; checking of extra-long-range communications with and control of the space station; more accurate calculation of the dimension of the solar system; a number of physical investigations in space.
- 1961 March 9 06:29 - Korabl-Sputnik 4 Launch Vehicle: Vostok 8K72K. Vostok 8K72K E103-14 Apogee: 239 km (148 mi). Carried dog Chernushka, mannequin Ivan Ivanovich, and other biological specimens. Ivanovich was ejected from the capsule and recovered by parachute, and Chernsuhka was successfully recovered with the capsule on March 9, 1961 8:10 GMT.
Officially: Development of the design of the space ship satellite and of the systems on board, which ensure necessary conditions for man's flight.
- 1961 March 25 05:54 - Korabl-Sputnik 5 Launch Vehicle: Vostok 8K72K. Vostok 8K72K E103-15 Apogee: 175 km (108 mi). Carried dog Zvezdochka and mannequin Ivan Ivanovich. Ivanovich was again ejected from the capsule and recovered by parachute, and Zvezdochka was successfully recovered with the capsule on March 25, 1961 7:40 GMT.
Officially: Development of the design of the space ship satellite and of the systems on board, designed to ensure man's life functions during flight in outer space and return to Earth.
- 1961 April 12 06:07 - Vostok 1 Launch Vehicle: Vostok 8K72K. Vostok 8K72K E103-16 Apogee: 315 km (195 mi). First manned spaceflight, one orbit of the earth. Three press releases were prepared, one for success, two for failures. It was only known ten minutes after burnout, 25 minutes after launch, if a stable orbit had been achieved.
The payload included life-support equipment and radio and television to relay information on the condition of the pilot. The flight was automated; Gagarin's controls were locked to prevent him from taking control of the ship. The combination to unlock the controls was available in a sealed envelope in case it became necessary to take control in an emergency. After retrofire, the service module remained attached to the Sharik reentry sphere by a wire bundle. The joined craft went through wild gyrations at the beginning of re-entry, before the wires burned through. The Sharik, as it was designed to do, then naturally reached aerodynamic equilibrium with the heat shield positioned correctly.
Gagarin ejected after re-entry and descended under his own parachute, as was planned. However for many years the Soviet Union denied this, because the flight would not have been recognized for various FAI world records unless the pilot had accompanied his craft to a landing. Recovered April 12, 1961 8:05 GMT. Landed Southwest of Engels Smelovka, Saratov.
- 1961 August 6 06:00 - Vostok 2 Launch Vehicle: Vostok 8K72K. Vostok 8K72K E103-17 Apogee: 221 km (137 mi). Second manned orbital flight. The Soviet Union successfully launched Vostok II into orbit with Gherman S. Titov as pilot. The spacecraft carried life-support equipment, radio and television for monitoring the condition of the cosmonaut, tape recorder, telemetry system, biological experiments, and automatic and manual control equipment. Flight objectives: Investigation of the effects on the human organism of a prolonged flight in orbit and subsequent return to the surface of the Earth; investigation of man's ability to work during a prolonged period of weightlessness. Titov took manual control of spacecraft but suffered from space sickness. He was equipped with a professional quality Konvas movie camera, with which ten minutes of film of the earth were taken through the porthole. Both television and film images were taken of the interior of the spacecraft. Like Gagarin, Titov experienced problems with separation of the service module after retrofire. Titov was never to fly again, after being assigned to the Spiral spaceplane, which turned out to be a dead-end project. A biography of him by Martin Caidin ('I Am Eagle') made him somewhat more accessible than Gagarin to the West.
- 1961 December 11 09:39 - Zenit-2 11F61 s/n 1 Launch Vehicle: Vostok 8K72K. RO-7 engine of block E upper stage cutoff prematurely. Spacecraft liquidated by self destruct system APO in 407th second of flight. Debris landed 100 km north of Vilyuisk.. First attempted launch of Zenit photo-reconnaisance satellite. According to Kamanin, there was a problem with the third stage, and the capsule landed between Novosibirsk and Yakutsk, but could not be located. There was no information on the nature of the problem. Korolev stayed at Tyuratam, preparing for the next launch attempt.
- 1962 - Operational Test mission Launch Vehicle: R-7A. Apogee: 1,000 km (600 mi).
- 1962 April 26 10:02 - Cosmos 4 Launch Vehicle: Vostok 8K72K. Apogee: 317 km (196 mi). Area survey photo reconnaissance satellite. Program partially completed. Failure of primary spacecraft orientation system. It was to spend four days in space, to be followed by another mission during 5-10 May. This meant that Vostok 3/4 could not be launched before 20-30 May. The cosmonaut prime crew returned from their in-suit parachute training at Fedosiya.
- 1962 June 1 09:38 - Zenit-2 11F61 s/n 3 Launch Vehicle: Vostok 8A92. Shutdown of Block B strap-on engine stage 1.8 seconds after liftoff. The booster crashed 300 m from the pad. Pad damaged.. Vostok 8A92 E15000-01 Area survey photo reconnaissance satellite. Third attempted launch of Zenit photo-reconnaissance satellite. It blew up 300 m from the pad, and did enough damage to put the launch complex out of operation for a month. Therefore the Vostok 3/4 launches could not take place until the end of July at the earliest.
- 1962 July 28 09:18 - Cosmos 7 Launch Vehicle: Vostok 8A92. Vostok 8A92 T15000-07 Apogee: 356 km (221 mi). Area survey photo reconnaissance satellite. Also performed radiation measurements.
- 1962 August 11 08:30 - Vostok 3 Launch Vehicle: Vostok 8K72K. Apogee: 218 km (135 mi). Joint flight with Vostok 4. The first such flight, where Vostok capsules were launched one day apart, coming within a few kilometers of each other at the orbital insertion of the second spacecraft. The flight was supposed to occur in March, but following various delays, one of the two Vostok pads was damaged in the explosion of the booster of the third Zenit-2 reconnsat in May. Repairs were not completed until August. Vostok 3 studied man's ability to function under conditions of weightlessness; conducted scientific observations; furthered improvement of space ship systems, communications, guidance and landing. Immediately at orbital insertion of Vostok 4, the spacecraft were less than 5 km apart. Popovich made radio contact with Cosmonaut Nikolayev. Nikolayev reported shortly thereafter that he had sighted Vostok 4. Since the Vostok had no maneuvering capability, they could not rendezvous or dock, and quickly drifted apart. The launches did allow Korolev to offer something new and different, and gave the launch and ground control crews practice in launching and handling more than one manned spacecraft at a time. The cosmonaut took colour motion pictures of the earth and the cabin interior.
- 1962 August 12 08:02 - Vostok 4 Launch Vehicle: Vostok 8K72K. Apogee: 211 km (131 mi). Joint flight with Vostok 3. Acquisition of experimental data on the possibility of establishing a direct link between two space ships; coordination of astronauts' operations; study of the effects of identical spaceflight conditions on the human organism. The launch of Popovich proceeds exactly on schedule, the spacecraft launching with 0.5 seconds of the planned time, entering orbit just a few kilometers away from Nikolayev in Vostok 3. Popovich had problems with his life support system, resulting in the cabin temperature dropping to 10 degrees Centigrade and the humidity to 35%. The cosmonaut still managed to conduct experiments, including taking colour motion pictures of the terminator between night and day and the cabin interior.
Despite the conditions, Popovich felt able to go for the full four days scheduled. But before the mission, Popovich had been briefed to tell ground control that he was 'observing thunderstorms' if he felt the motion sickness that had plagued Titov and needed to return on the next opportunity. Unfortunately he actually did report seeing thunderstorms over the Gulf of Mexico, and ground control took this as a request for an early return. He was ordered down a day early, landing within a few mintutes of Nikolayev. Only on the ground was it discovered that he was willing to go the full duration, and that ground control had thought he had given the code.
- 1962 August 25 02:18 - Sputnik 19 Launch Vehicle: Molniya 8K78. At T+60 min 50 sec one of the four solid motors of the escape stage's BOZ unit did not fire. The resulting asymmetric torque caused the stage to lose correct attitude and three seconds after ignition of the main engine S1.5400A1 it began to tumble.. Molniya 8K78 T103-12 Apogee: 252 km (156 mi). Attempt to launch a probe towards Mars. The launch went well, but the fourth stage motor burnt for only 45s of the planned 240s. The stage remained in Earth orbit. However Kamanin notes that it was good that the launch of the basic vehicle was a success - it gave the visiting female cosmonauts confidence in the rocket they will have to ride.
- 1962 September 1 02:12 - Sputnik 20 Launch Vehicle: Molniya 8K78. At T+ 61 min 30 sec the fuel valve did not open.; the ignition command was blocked from going to the main engine of Stage 4.. Molniya 8K78 T103-13 Apogee: 246 km (152 mi).
- 1962 September 12 00:59 - Sputnik 21 Launch Vehicle: Molniya 8K78. At T+531 sec, the fourth vernier chamber of Stage 3's 8D715K engine exploded because the LOX cut-off valve had not closed as scheduled and LOX flowed into the hot chamber.. Molniya 8K78 T103-14 Apogee: 218 km (135 mi). The escape stage entered parking orbit but the main engine cut off just 0.8 s after ignition due to cavitation in the oxidiser pump and pump failure.
- 1962 September 27 09:39 - Cosmos 9 Launch Vehicle: Vostok 8A92. Vostok 8A92 T15000-06 Apogee: 981 km (609 mi). Area survey photo reconnaissance satellite. Also performed radiation measurements.
- 1962 October 17 09:00 - Cosmos 10 Launch Vehicle: Vostok 8A92. Vostok 8A92 T15000-03 Apogee: 376 km (233 mi). Area survey photo reconnaissance satellite. Also performed radiation measurements.
- 1962 October 24 17:55 - Sputnik 22 Launch Vehicle: Molniya 8K78. 16 seconds after ignition of Stage 4, Block L's S1.5400A1 engine exploded. A lubricant leak resulted in the jamming of a shaft in the turbopump gearbox and break up of the turbine.. Molniya 8K78 T103-15 Apogee: 260 km (160 mi). Mars probe intended to photograph Mars on a flyby trajectory. The spacecraft broke into many pieces, some of which apparently remained in Earth orbit for a few days. This occurred during the Cuban missile crisis and was picked up by U.S. military radar installations, who originally feared it might by the start of a Soviet nuclear attack.
- 1962 November 1 16:14 - Mars 1 Launch Vehicle: Molniya 8K78. Molniya 8K78 T103-16 Mars probe intended to photograph Mars on a flyby trajectory. Launched from Sputnik 23 in a 157 x 238 km, 65 degree parking orbit. Sixty-one radio transmissions were held in which a large amount of data was collected. On March 21, 1963, when the spacecraft was at a distance of 106 million km communications ceased, possibly due to a malfunction in the spacecraft orientation system. Mars 1 closest approach to Mars occurred on June 19, 1963 at a distance of approximately 193,000 km, after which the spacecraft entered a heliocentric orbit. Announced mission: Prolonged exploration of outer space during flight to the planet Mars; establishment of inter-planetary radio communications; photgraphing of the planet Mars and subsquent radio-transmission to Earth of the photographs of the surface of Mars thus obtained.
- 1962 November 4 15:35 - Sputnik 24 Launch Vehicle: Molniya 8K78. After T+260 sec, a malfunction of the pressurisation system of the central sustainer led to cavitation in the oxidiser pipeline and LOX pump, followd at T+292s by the fuel pump.. Molniya 8K78 T103-17 Apogee: 170 km (100 mi). Mars probe intended to make a soft landing on Mars. Although the escape stage and payload reached orbit, the strong third stage vibrations shook a fuse loose from its mount in the main nozzle of the escape stage Block L's engine. The engine could not be ignited and remained in Earth orbit. It decayed about two months after insertion.
- 1962 December 22 09:23 - Cosmos 12 Launch Vehicle: Vostok 8A92. Vostok 8A92 T15000-10 Apogee: 385 km (239 mi). Area survey photo reconnaissance satellite. Also performed radiation measurements.
- 1963 January 4 08:49 - Sputnik 25 Launch Vehicle: Molniya 8K78. The escape stage's BOZ unit failed to operate due to failure of a DC transformer of the power system. The stage with payload remained in Earth orbit.. Molniya 8K78/E6 T103-09 Apogee: 189 km (117 mi).
- 1963 February 3 09:29 - E-6 s/n 2 failure. Launch Vehicle: Molniya 8K78. Upper stage gyro platform failure.. Molniya 8K78/E6 G103-10 Apparent causes were instabilities in the torque sensor circuit and the pitch-free floating gyro device. The upper stages and payload broke up on re-entry into the atmosphere over the Pacific.
- 1963 March 21 08:30 - Cosmos 13 Launch Vehicle: Vostok 8A92. Vostok 8A92 T15000-01 Apogee: 303 km (188 mi). Area survey photo reconnaissance satellite. Also performed radiation measurements.
- 1963 April 2 08:16 - Luna 4 Launch Vehicle: Molniya 8K78. Molniya 8K78/E6 G103-11 Apogee: 182 km (113 mi). Luna 4 was the second attempted Soviet unmanned lunar soft lander probe. The spacecraft, rather than being sent on a straight trajectory toward the Moon, was placed first in an earth parking orbit. The rocket stage then reignited and put the spaccecraft on a translunar trajectory. Failure of Luna 4 to make a required midcourse correction resulted in it missing the Moon by 8336.2 km on April 6, at 4:26 a.m. Moscow time. It thereafter entered a barycentric Earth orbit. The Soviet news agency, Tass, reported that data had been received from the spacecraft throughout its flight and that radio communication would continue for a few more days.
- 1963 April 22 08:30 - Cosmos 15 Launch Vehicle: Vostok 8A92. Vostok 8A92 T15000-08 Apogee: 336 km (208 mi). Area survey photo reconnaissance satellite. Also carried weather, radiation experiments.
- 1963 April 28 08:50 - Cosmos 16 Launch Vehicle: Vostok 8A92. Vostok 8A92 E15000-02 Apogee: 379 km (235 mi). Program partially completed. Part of the information lost due to failure of engine block stabilization system. Area survey photo reconnaissance satellite. Also performed radiation measurements.
- 1963 May 24 10:33 - Cosmos 18 Launch Vehicle: Vostok 8A92. Vostok 8A92 E15000-12 Apogee: 269 km (167 mi). Area survey photo reconnaissance satellite. Also performed radiation measurements.
- 1963 June 14 11:58 - Vostok 5 Launch Vehicle: Vostok 8K72K. Apogee: 131 km (81 mi). Joint flight with Vostok 6. The Soviet Union launched Vostok 5, piloted by Lt. Col. Valery F. Bykovsky. Two days later Lt. Valentina V. Tereshkova, the first spacewoman, followed in Vostok 6. On its first orbit, Vostok 6 came within about five km of Vostok 5, the closest distance achieved during the flight, and established radio contact. Both cosmonauts landed safely on June 19. The space spectacular featured television coverage of Bykovsky that was viewed in the West as well as in Russia. Unlike earlier missions, only a black and white film camera was carried. Photometric measurements of the earth's horizon were made.
Mission objectives were officially: further study of the effect of various space-flight factors in the human organism; extensive medico-biological experiments under conditions of prolonged flight; further elaboration and improvement of spaceship systems.
Vostok 5 was originally planned to go for a record eight days. The launch was delayed repeatedly due to high solar activity and technical problems. Finally the spacecraft ended up in a lower than planned orbit. Combined with increased atmospheric activity due to solar levels, Vostok 5 quickly decayed temperatures in the service module reached very high levels.
Bykovsky also experienced an unspecified problem with his waste management system (a spill?) which made conditions in the cabin 'very uncomfortable'. He was finally ordered to return after only five days in space.
To top it all off, once again the Vostok service module failed to separate cleanly from the reentry sphere. Wild gyrations ensued until the heat of reentry burned through the non-separating retraining strap.
- 1963 June 16 09:29 - Vostok 6 Launch Vehicle: Vostok 8K72K. Apogee: 166 km (103 mi). Joint flight with Vostok 5. First woman in space, and the only Russian woman to go into space until Svetlana Savitskaya 19 years later. On its first orbit, Vostok 6 came within about five km of Vostok 5, the closest distance achieved during the flight, and established radio contact. Flight objectives included: Comparative analysis of the effect of various space-flight factors on the male and female organisms; medico-biological research; further elaboration and improvement of spaceship systems under conditions of joint flight. It was Korolev's idea just after Gagarin's flight to put a woman into space as yet another novelty. Khrushchev made the final crew selection. Korolev was unhappy with Tereshkova's performance in orbit and she was not permitted to take manual control of the spacecraft as had been planned.
- 1963 July 10 - Zenit-2 11F61 s/n 12 Launch Vehicle: Vostok 8A92. Shutdown of Block B strap-on engine stage 1.9 seconds after liftoff. Pad damaged.. Vostok 8A92 E15000-04 Area survey photo reconnaissance satellite.
- 1963 October 18 09:29 - Cosmos 20 Launch Vehicle: Vostok 8A92. Vostok 8A92 G15001-01 Apogee: 296 km (183 mi). Area survey photo reconnaissance satellite.
- 1963 November 11 06:23 - Cosmos 21 Launch Vehicle: Molniya 8K78. During unpowered coast in parking orbit the escape stage Block L lost stable attitude. Engine ignition occurred in an incorrect direction.. Molniya 8K78 G103-18 Apogee: 231 km (143 mi). The stage with payload remained in Earth orbit as Cosmos-51 and burnt up on re-entry.
- 1963 November 16 10:34 - Cosmos 22 Launch Vehicle: Voskhod 11A57. Voskhod 11A57 G15000-06 Apogee: 376 km (233 mi). High resolution photo reconnaissance satellite; returned film capsule
- 1963 November 28 - Zenit-2 11F61 s/n 14 Launch Vehicle: Vostok 8A92. Failure of block E upper stage. Spacecraft liquidated by APO destruct system.. Vostok 8A92 G15001-02 Area survey photo reconnaissance satellite.
- 1963 December 19 09:28 - Cosmos 24 Launch Vehicle: Vostok 8A92. Vostok 8A92 G15001-03 Apogee: 391 km (242 mi). Area survey photo reconnaissance satellite.
- 1964 January 30 09:45 - Elektron 1 Launch Vehicle: Vostok 8K72K. Apogee: 6,439 km (4,001 mi). Studied inner Van Allen belt. Electron I and II launched by a single carrier rocket. Electron I: simultaneous study of the Earth's inner and outer radiation belts, cosmic rays and upper atmosphere. Electron II: simultaneous study of the Earth's inner and outer radiation belts, cosmic rays and outer space.
- 1964 February 19 05:47 - 3MV-1A Launch Vehicle: Molniya 8K78M. Second stage failure.. Molniya 8K78M T15000-19
- 1964 March 21 08:15 - Luna failure Launch Vehicle: Molniya 8K78M. Failure. Molniya 8K78M T15000-20 The upper stages burnt on re-entry into the atmosphere.
- 1964 March 27 03:24 - Cosmos 27 Launch Vehicle: Molniya 8K78M. During unpowered coast in parking orbit the escape stage Block L lost stable attitude due to a loss of the the power circuit of the pneumatic valves of the attitude control and stabilisation system.. Molniya 8K78M T15000-22 Apogee: 209 km (129 mi). The stage with payload remained in Earth orbit as Cosmos-27.
- 1964 April 2 02:42 - Zond 1 Launch Vehicle: Molniya 8K78M. Molniya 8K78M T15000-23 Failed Venus probe. Solar Orbit (Heliocentric). Elaboration of a long range space system and conduct of scientific research.
- 1964 April 20 08:08 - Luna failure Launch Vehicle: Molniya 8K78M. Power failure caused upper stage shutdown at T+340 seconds.. Molniya 8K78M T15000-21 The upper stages broke up on re-entry into the atmosphere..
- 1964 May 18 09:50 - Cosmos 30 Launch Vehicle: Voskhod 11A57. Voskhod 11A57 G15000-12 Apogee: 366 km (227 mi). High resolution photo reconnaissance satellite; returned film capsule
- 1964 June 4 - Molniya-1 s/n 2 Failure Launch Vehicle: Molniya 8K78. At T+104 sec the tank draining of core Block A failed due to jamming of the servo-motored throttle and break down of the motor's circuit The launcher was destroyed on impact downrange from the pad.. Molniya 8K78 R103-34 Unsuccessful first attempt to launch Molniya communications satellite.
- 1964 July 1 11:16 - Cosmos 34 Launch Vehicle: Voskhod 11A57. Voskhod 11A57 T15000-04 Apogee: 342 km (212 mi). High resolution photo reconnaissance satellite; returned film capsule
- 1964 July 10 21:51 - Elektron 3 Launch Vehicle: Vostok 8K72K. Apogee: 6,302 km (3,915 mi). Studied inner Van Allen belt. Electron 3 and 4 launched by a single carrier rocket. Simultaneous study of the inner and outer radiation belts of the earth, cosmic rays and the upper atmosphere.
- 1964 August 22 07:12 - Cosmos 41 Launch Vehicle: Molniya 8K78. Molniya 8K78 R103-36 Apogee: 39,169 km (24,338 mi). Successful launch of first Soviet communications satellite. This is the second Molniya launch attempt. (the first was a launch failure). The failure of the antennae to deploy means the spacecraft can only be tested in a limited manner and cannot be used for the planned relay of television.
- 1964 September 13 09:50 - Cosmos 45 Launch Vehicle: Voskhod 11A57. Voskhod 11A57 R15001-01 Apogee: 311 km (193 mi). High resolution photo reconnaissance satellite; returned film capsule; also carried weather experiments. The Zenit-4 launches a day ahead of schedule. The booster rocket performs perfectly as Korolev and Kamanin watch from the veranda of the IP-1 tracking station. This confirms readiness of the same launch vehicle for the Voskhod launch.
- 1964 October 12 07:30 - Voskhod 1 Launch Vehicle: Voskhod 11A57. Voskhod 11A57 R15000-04 Apogee: 336 km (208 mi). The U.S.S.R. launched the world's first multi-manned spacecraft, Voskhod I, the first to carry a scientist and a physician into space. The crew were Col. Vladimir Komarov, pilot; Konstantin Feoktistov, scientist; and Boris Yegorov, physician. Potentially dangerous modification of Vostok to upstage American Gemini flights; no spacesuits, ejection seats, or escape tower. One concession was backup solid retrorocket package mounted on nose of spacecraft. Seats mounted perpendicular to Vostok ejection seat position, so crew had to crane their necks to read instruments, still mounted in their original orientation. Tested the new multi-seat space ship; investigated the in-flight work potential and co-operation of a group of cosmonauts consisting of specialists in different branches of science and technology; conducted scientific physico-technical and medico-biological research. The mission featured television pictures of the crew from space.
Coming before the two-man Gemini flights, Voskhod 1 had a significant worldwide impact. In the United States, the "space race" was again running under the green flag. NASA Administrator James E. Webb, commenting on the spectacular, called it a "significant space accomplishment." It was, he said, "a clear indication that the Russians are continuing a large space program for the achievement of national power and prestige."
- 1964 November 30 13:12 - Zond 2 Launch Vehicle: Molniya 8K78. Mars probe intended to photograph Mars on a flyby trajectory. Zond 2 was launched from an earth parking orbit towards Mars to test space-borne systems and to carry out scientific investigations. Zond 2 carried six electric rocket engines of plasma type that served as actuators of the attitude control system. The communications system failed during April 1965. The spacecraft flew by Mars on August 6, 1965, at a distance of 1500 km.
- 1965 March 12 09:30 - Cosmos 60 Launch Vehicle: Molniya 8K78. The escape stage Block L's engine failed to ignite due to failure of a transformer in the power supply of the control system.. Molniya 8K78/E6 R103-25 Apogee: 248 km (154 mi). The stage with the payload remained in Earth orbit as Kosmos-60.
- 1965 March 18 07:00 - Voskhod 2 Launch Vehicle: Voskhod 11A57. Voskhod 11A57 R15000-05 Apogee: 475 km (295 mi). First spacewalk, with a two man crew of Colonel Pavel Belyayev and Lt. Colonel Aleksey Leonov. During Voskhod 2's second orbit, Leonov stepped from the vehicle and performed mankind's first "walk in space." After 10 min of extravehicular activity, he returned safely to the spacecraft through an inflatable airlock.
This mission was originally named 'Vykhod ('Exit/Advance'). It almost ended in disaster when Leonov was unable to reenter the airlock due to stiffness of the inflated spacesuit. He had to bleed air from the suit in order to get into the airlock. After Leonov finally managed to get back into the spacecraft cabin, the primary hatch would not seal completely. The environmental control system compensated by flooding the cabin with oxygen, creating a serious fire hazard in a craft only qualified for sea level nitrogen-oxygen gas mixes (Cosmonaut Bondarenko had burned to death in a ground accident in such circumstances, preceding the Apollo 204 disaster by many years).
- 1965 April 10 - Luna failure - stage 3 engine failure. Launch Vehicle: Molniya 8K78. Stage 3's engine 8D715K failed due to depressurisation of the nitrogen pipeline of the LOX tank pressurisation system of Block I.. Molniya 8K78 R103-26 The upper stages fell apart on re-entry into the atmosphere..
- 1965 April 23 01:55 - Molniya 1-01 Launch Vehicle: Molniya 8K78. Molniya 8K78 U103-35 Apogee: 39,300 km (24,400 mi). First announced launch of Soviet communications satellite. Television programme transmission and long range two way multi channel telephone and telegraph communications. Orbital characteristics after correction of 2 May 1965.
- 1965 May 9 07:49 - Luna 5 Launch Vehicle: Molniya 8K78M. Molniya 8K78M U103-30 Apogee: 219 km (136 mi). Soft lunar landing attempt. The retrorocket system failed, and the spacecraft impacted the lunar surface at the Sea of Clouds. Western observers, among them England's Sir Bernard Lovell, correctly speculated that the craft's mission was a soft landing.
- 1965 June 8 07:40 - Luna 6 Launch Vehicle: Molniya 8K78M. Molniya 8K78M U103-31 Attempted unmanned lunar soft lander. Tass reported that all onboard equipment was functioning normally. Two days into the flight, however, the spacecraft's engine failed to shut down following a midcourse correction. This failure caused Luna 6 to miss its target by 159,612.8 Km.
- 1965 June 25 09:50 - Cosmos 69 Launch Vehicle: Voskhod 11A57. Voskhod 11A57 G15000-10 Apogee: 310 km (190 mi). High resolution photo reconnaissance satellite; returned film capsule
- 1965 July 18 14:38 - Zond 3 Launch Vehicle: Molniya 8K78. Zond 3 was towards the moon and interplanetary space. The spacecraft was equipped with a TV system that provided automatic inflight film processing. On July 20, during lunar flyby, 25 pictures of very good quality were taken of the lunar farside from distances of 11,570 to 9960 km. The photos covered 19,000,000 km square of the lunar surface. Photo transmissions by facsimile were returned to earth from a distance of 2,200,000 km on July 29 and were retransmitted later from a distance of 31,500,000 km, thus proving the ability of the communications system. After the lunar flyby, Zond 3 continued space exploration in a heliocentric orbit. Those pictures showed clearly the heavily cratered nature of the surface. This mission dramatized the advances in space photography that the U.S.S.R. had made since its first far-side effort six years earlier.
- 1965 August 25 10:19 - Cosmos 79 Launch Vehicle: Voskhod 11A57. Voskhod 11A57 R15001-06 Apogee: 338 km (210 mi). High resolution photo reconnaissance satellite; returned film capsule
- 1965 October 4 07:56 - Luna 7 Launch Vehicle: Molniya 8K78. Molniya 8K78 U103-27 Lunar soft landing attempt. The Luna 7 spacecraft was intended to achieve a soft landing on the Moon. However, due to premature retrofire and cutoff of the retrorockets, the spacecraft impacted the lunar surface in the Sea of Storms.
- 1965 October 14 19:40 - Molniya 1-02 Launch Vehicle: Molniya 8K78. Molniya 8K78 U103-37 Apogee: 39,921 km (24,805 mi). France - USSR communications link. Second communications satellite 'Molniya-1'. Television programme transmission and long-range, two-way multi-channel telephone, phototelegraph and telegraph communications.
- 1966 August 27 09:50 - Cosmos 128 Launch Vehicle: Voskhod 11A57. Voskhod 11A57 N15001-03 Apogee: 343 km (213 mi). High resolution photo reconnaissance satellite; returned film capsule
- 1966 October 20 07:55 - Molniya 1-04 Launch Vehicle: Molniya 8K78M. Molniya 8K78M N103-40 Apogee: 39,689 km (24,661 mi). Television programme transmission and long-range two-way multi-channel telephone, phototelegraph and telegraph communicaitons.
- 1966 December 21 10:17 - Luna 13 Launch Vehicle: Molniya 8K78M. Molniya 8K78M N103-45 Soft landed on Moon 24 December 1966 at 18:01:00 GMT, Latitude 18.87 N, 297.95 E - Oceanus Procellarum. The petal encasement of the spacecraft was opened, antennas were erected, and radio transmissions to Earth began four minutes after the landing. On December 25 and 26, 1966, the spacecraft television system transmitted panoramas of the nearby lunar landscape at different sun angles. Each panorama required approximately 100 minutes to transmit. The spacecraft was equipped with a mechanical soil-measuring penetrometer, a dynamograph, and a radiation densitometer for obtaining data on the mechanical and physical properties and the cosmic-ray reflectivity of the lunar surface. It is believed that transmissions from the spacecraft ceased before the end of December 1966.
- 1967 February 7 03:20 - Cosmos 140 Launch Vehicle: Soyuz 11A511. Soyuz 11A511 U15000-03 Apogee: 216 km (134 mi). After the self-destruction of the first Soyuz 7K-OK on re-entry, and the loss of the second one on the pad fire in December, the state commission ruled that the third 7K-OK model would be flown unpiloted on a solo mission. If this was successful then the fourth and fifth Soyuz would be flown on a manned docking mission. Once in orbit Cosmos 140 experienced attitude control problems due to a faulty star sensor resulting in excessive fuel consumption. The spacecraft couldn't keep the required orientation towards the sun to keep the solar panels illuminated, and the batteries discharged. Despite all of these problems the spacecraft remained controllable. An attempted manoeuvre on the 22nd revolution still showed problems with the control system. It malfunctioned yet again during retrofire, leading to a steeper than planned uncontrolled ballistic re-entry. The re-entry capsule itself had depressurised on separation from the service module due to a fault in the base of the capsule. A 300 mm hole burned through in the heat shield during re-entry. Although such events would have been lethal to any human occupants, the capsule's recovery systems operated and the capsule crashed through the ice of the frozen Aral Sea, 3 km from shore and 500 kilometres short of the intended landing zone. The spacecraft finally sank in 10 meters of water and had to be retrieved by divers. Still, the mission was deemed 'good enough' for the next mission to be a manned two-craft docking and crew transfer space spectacular. Mishin and Kamanin felt that a human crew could have sorted out the problems. They were also under intense pressure to achieve a manned circumlunar flight before the 50th Anniversary of the Soviet Revolution in October.
- 1967 February 27 08:45 - Cosmos 143 Launch Vehicle: Vostok 8A92. Vostok 8A92 U15001-03 Apogee: 390 km (240 mi). Placed into orbit with 22.8 second period different from that planned. Area survey photo reconnaissance satellite. Also carried science package.
- 1967 April 12 10:51 - Cosmos 155 Launch Vehicle: Voskhod 11A57. Voskhod 11A57 N15001-08 Apogee: 267 km (165 mi). High resolution photo reconnaissance satellite; returned film capsule
- 1967 April 23 00:35 - Soyuz 1 Launch Vehicle: Soyuz 11A511. Soyuz 11A511 U15000-04 Apogee: 223 km (138 mi). Space disaster that put back Soviet lunar program 18 months. Soyuz 1 as active spacecraft was launched first. Soyuz 2, with a 3 man crew would launch the following day, with 2 cosmonauts spacewalking to Soyuz 1. However immediately after orbital insertion Komarov's problems started. One of the solar panels failed to deploy, staying wrapped around the service module. Although only receiving half of the planned solar power, an attempt was made to manoeuvre the spacecraft. This failed because of interference of the reaction control system exhaust with the ion flow sensors that were one of the Soyuz' main methods of orientation.
- 1967 May 12 10:30 - Cosmos 157 Launch Vehicle: Vostok 8A92. Apogee: 262 km (162 mi). Area survey photo reconnaissance satellite. Program partially completed. Bad quality film loaded into SA-20 camera.
- 1967 May 16 21:43 - Cosmos 159 Launch Vehicle: Molniya 8K78M. Molniya 8K78M Ya716-56 Apogee: 60,637 km (37,678 mi). The E-6LS was a radio-equipped version of the E-6 used to test tracking and communications networks for the Soviet manned lunar program. The payload entered the desired orbit as Kosmos-159.
- 1967 May 24 22:50 - Molniya 1-05 Launch Vehicle: Molniya 8K78M. Apogee: 35,690 km (22,170 mi). Further development and experimental operation of long-range two-way television and telephone-telegraph radio-communication.
- 1967 June 1 10:40 - Cosmos 162 Launch Vehicle: Voskhod 11A57. Voskhod 11A57 Ya15001-11 Apogee: 275 km (170 mi). High resolution photo reconnaissance satellite; returned film capsule
- 1967 June 12 02:39 - Venera 4 Launch Vehicle: Molniya 8K78M. Venera 4 was successfully launched towards the planet Venus with the announced mission of direct atmospheric studies. On October 18, 1967, the descent vehicle entered the Venusian atmosphere. Signals were returned by the spacecraft, which deployed a parachute after braking to subsonic velocity in the Venusian atmosphere, until it reached an altitude of 24.96 km.
- 1967 June 17 02:36 - Cosmos 167 Launch Vehicle: Molniya 8K78M. Stage 4's engine 11D33 failed to ignite because the turbopump had not been cooled before ignition.. Apogee: 264 km (164 mi). Suggestions for the cause of the failure included incorrect soldering of wires in multiple pin plugs, wrong attachments of the plugs to the pyrotechnic connectors, or a mix-up of the pyrotechnic connectors during assembly.. Investigation of the upper atmosphere and outer space.
- 1967 September 16 06:06 - Cosmos 177 Launch Vehicle: Voskhod 11A57. Apogee: 267 km (165 mi). Area survey photo reconnaissance satellite.
- 1967 October 30 08:12 - Cosmos 188 Launch Vehicle: Soyuz 11A511. Apogee: 247 km (153 mi). Docking target craft for Cosmos 186, which achieved world's first automatic rendezvous on second attempt. Hard docking achieved but electric connections unsuccessful due to misallignment of spacecraft. Ion flow sensor failed and Cosmos 188 had to make a high-G uncontrolled re-entry. When it deviated too far off course, it was destroyed by the on-board self-destruct system,. However officially the Soviet Union reported that it landed succesfully on November 2, 1967 at 09:10 GMT, and that its mission was 'investigation of outer space, development of new systems and elements to be used in the construction of space devices'.
- 1968 February 7 10:43 - E-6LS s/n 112 Launch Vehicle: Molniya 8K78M. At T+524.6 sec Stage 3's engine 11D55 cut off prematurely because it ran out of fuel due to an excessive fuel consumption rate through the gas-generator.. Molniya 8K78M Ya716-57 Failed launch of an E-6LS radio-equipped version of the E-6 used to test tracking and communications networks for the Soviet manned lunar program. Suggestions for the abnormal consumption included the seizing up of a pintle valve for controlling fuel supply into the regulator or the seizing up of the fuel inlet control. The upper stages broke up in the atmosphere.
- 1968 March 21 09:50 - Cosmos 208 Launch Vehicle: Voskhod 11A57. Apogee: 287 km (178 mi). Area survey photo reconnaissance satellite; returned film capsule; deployed high energy gamma ray experiment capsule. First flight of modernised Zenit-2 area survey reconnaissance satellite.
- 1968 April 7 10:09 - Luna 14 Launch Vehicle: Molniya 8K78M. Molniya 8K78M Ya716-58 Lunar Orbiter; studied lunar gravitational field, Earth-Moon gravitational relationship, and conducted further scientific experiments in circumlunar space. Not revealed until years later was that the E-6LS was primarily intended to test tracking and communications networks for the Soviet manned lunar program. The Luna 14 spacecraft entered a 140 x 870 km x 42 degree lunar orbit on April 10, 1966. The spacecraft instrumentation was similar to that of Luna 10 and provided data for studies of the interaction of the earth and lunar masses, the lunar gravitational field, the propagation and stability of radio communications to the spacecraft at different orbital positions, solar charged particles and cosmic rays, and the motion of the Moon. This flight was the final flight of the second generation of the Luna series.
- 1968 April 15 09:34 - Cosmos 213 Launch Vehicle: Soyuz 11A511. Apogee: 254 km (157 mi). Cosmos 213 was the target for Cosmos 212 in a successful test of Soyuz 7K-OK rendezvous and docking systems. The Cosmos 213 launch was the most accurate yet. The spacecraft was placed in orbit only 4 km from Cosmos 212, ready for a first-orbit docking. Both spacecraft were recovered, but Cosmos 213 was dragged by heavy wind across the steppes when the parachute lines didn't jettison at touchdown. This failure caused the upcoming Soyuz 2/3 manned docking mission to be scaled back.
Officially: Investigation of outer space, development of new systems and elements to be used in the construction of space devices.
- 1968 June 21 12:00 - Cosmos 228 Launch Vehicle: Voskhod 11A57. Apogee: 245 km (152 mi). Area survey photo reconnaissance satellite; returned film capsule; deployed cosmic ray experiment capsule.
- 1968 September 23 07:39 - Cosmos 243 Launch Vehicle: Voskhod 11A57. Apogee: 293 km (182 mi). Area survey photo reconnaissance satellite; returned film capsule; deployed passive microwave radio telescope capsule.
- 1968 October 25 09:00 - Soyuz 2 Launch Vehicle: Soyuz 11A511. Apogee: 229 km (142 mi). Unmanned docking target for Soyuz 3. Soyuz 2 launched on time at 12:00 local time, in 0 deg C temperatures and 5 m/s winds. Launch was on time 'as in Korolev's time', notes Kamanin. Docking with Soyuz 3 a failure. Recovered October 28, 1968 7:51 GMT, 5 km from its aim point. Maneuver Summary:
177km X 196km orbit to 184km X 230km orbit. Delta V: 12 m/s.
Officially: Complex testing of spaceship systems in conditions of space flight.
- 1968 October 31 - Cosmos 251 Launch Vehicle: Voskhod 11A57. Apogee: 255 km (158 mi). High resolution photo reconnaissance satellite; returned film capsule; deployed radio astronony and gamma ray experiment capsule; maneuverable.
- 1969 January 15 07:04 - Soyuz 5 Launch Vehicle: Soyuz 11A511. Apogee: 212 km (131 mi). At 3 am an An-12 arrives from Moscow with ten newspapers, and letters for Shatalov, to be delivered by the Soyuz 5 crew to him as the first 'space mail'. At 05:15 the State Commission convened and approved launch at 10:04:30. The countdown proceeds normally; meanwhile communications sessions are held with Shatalov on Soyuz 4. The commission is taken by automobile convoy from Area 2, to Area 17, where the Soyuz 5 crew declares itself ready for flight. At T-25 minutes, with the crew already aboard the spacecraft, a piece of electrical equipment fails and needs to be replaced. Engineer-Captain Viktor Vasilyevich Alyeshin goes to the fuelled booster and replaces it. While doing this he notices that the access hatch has been secured with only three bolts, instead of the four required. Nevertheless the launch proceeds successfully. After Soyuz 5 is in orbit, it and Soyuz 4 begin their mutual series of manoeuvres for rendezvous and docking. Officially the flight conducted scientific, technical and medico-biological research, checking and testing of onboard systems and design elements of space craft, docking of piloted space craft and construction of an experimental space station, transfer of cosmonauts from one craft to another in orbit.
- 1969 January 23 09:15 - Cosmos 264 Launch Vehicle: Voskhod 11A57. Apogee: 295 km (183 mi). High resolution photo reconnaissance satellite; returned film capsule; carried radio astronony and gamma ray experiments; maneuverable.
- 1969 April 23 09:55 - Cosmos 280 Launch Vehicle: Voskhod 11A57. Apogee: 250 km (150 mi). High resolution photo reconnaissance satellite; returned film capsule; carried weather experiments; maneuverable.
- 1969 October 12 10:44 - Soyuz 7 Launch Vehicle: Soyuz 11A511. Apogee: 223 km (138 mi). Tested spacecraft systems and designs, manoeuvring of space craft with respect to each other in orbit, conducted scientific, technical and medico-biological experiments in group flight. Was to have docked with Soyuz 8 and transferred crew while Soyuz 6 took film from nearby. However failure of rendezvous electronics in all three craft due to a new helium pressurization integrity test prior to the mission did not permit successful rendezvous and dockings.
- 1971 April 22 23:54 - Soyuz 10 Launch Vehicle: Soyuz 11A511. Soyuz 11A511 25 Apogee: 258 km (160 mi). Intended first space station mission; soft docked with Salyut 1. Launch nearly scrubbed due to poor weather. Soyuz 10 approached to 180 m from Salyut 1 automatically. It was hand docked after faillure of the automatic system, but hard docking could not be achieved because of the angle of approach. Post-flight analysis indicated that the cosmonauts had no instrument to proivde the angle and range rate data necessary for a successful manual docking. Soyuz 10 was connected to the station for 5 hours and 30 minutes. Despite the lack of hard dock, it is said that the crew were unable to enter the station due to a faulty hatch on their own spacecraft. When Shatalov tried to undock from the Salyut, the jammed hatch impeded the docking mechanism, preventing undocking. After several attempts he was unable to undock and land.
- 1971 June 6 04:55 - Soyuz 11 Launch Vehicle: Soyuz 11A511. Apogee: 237 km (147 mi). First space station flight, two years before the American Skylab. The Soyuz 11 launch proceeds without any difficulties. The first orbital correction in the set of rendezvous manoeuvres to head for Salyut 1 is made on the fourth revolution. At 15:00 Kamanin and other critical staff board a plane for the mission control centre at Yevpatoriya. The aircraft takes 4 hours 30 minutes to get there.
Equipment aboard Salyut 1 included a telescope, spectrometer, electrophotometer, and television. The crew checked improved on-board spacecraft systems in different conditions of flight and conducted medico-biological research. The main instrument, a large solar telescope, was inoperative because its cover failed to jettison. A small fire and difficult working conditions will lead to a decision to return crew before planned full duration of 30 days.
- 1972 June 26 14:53 - Cosmos 496 Launch Vehicle: Soyuz 11A511. Apogee: 253 km (157 mi). Recovered July 6, 1972 13:54 GMT. Soyuz 7K-T redesign test.
- 1973 June 15 06:00 - Cosmos 573 Launch Vehicle: Soyuz 11A511. Apogee: 308 km (191 mi). Soyuz test flight. Recovered June 17, 1973 6:01 GMT. Soyuz 7K-T redesign test, probably using one of the spacecraft allocated to the failed Salyut 2 or Cosmos 557 stations.
- 1973 September 27 12:18 - Soyuz 12 Launch Vehicle: Soyuz 11A511. Apogee: 348 km (216 mi). Experimental flight for the purpose of further development of manned space craft Soyuz 7K-T modifications. After the Soyuz 11 disaster, the Soyuz underwent redesign for increased reliability. Two solo test flights of the new design were planned. Crews for the first flight were those already planned for the deferred follow-on missions to the failed DOS 2 and DOS 3 space stations.
- 1973 November 30 05:20 - Cosmos 613 Launch Vehicle: Soyuz 11A511. Apogee: 276 km (171 mi). Unmanned Soyuz test flight. Recovered January 29, 1974 5:29 GMT. Soyuz 7K-T duration test.
- 1973 December 18 11:55 - Soyuz 13 Launch Vehicle: Soyuz 11A511. Apogee: 247 km (153 mi). A unique flight of the 7K-T/AF modification of the Soyuz spacecraft. The orbital module was dominated by the large Orion 2 astrophysical camera. The crew conducted astrophysical observations of stars in the ultraviolet range. Additional experiments included spectrozonal photography of specific areas of the earth's surface, and continued testing of space craft's on-board systems.
- 1974 May 27 07:20 - Cosmos 656 Launch Vehicle: Soyuz 11A511. Apogee: 364 km (226 mi). Unmanned test flight of the Soyuz 7K-T(A9) Soyuz variant designed for docking with the military Almaz space station. Recovered May 29, 1974 7:50 GMT.
- 1974 July 3 18:51 - Soyuz 14 Launch Vehicle: Soyuz 11A511. Apogee: 217 km (134 mi). On 4 July Soyuz 14 docked with the Salyut 3 space station after 15 revolutions of the earth. The planned experimental program included manned military reconnaissance of the earth's surface, assessing the fundamental value of such observations, and some supplemental medico-biological research. After the crew's return research continued in the development of the on-board systems and the principles of remote control of such a station.
- 1974 August 6 00:02 - Cosmos 670 Launch Vehicle: Soyuz 11A511U. Apogee: 294 km (182 mi). Unmanned Soyuz 7K-S test flight. Recovered August 8, 1974 23:59 GMT.
- 1974 August 26 19:58 - Soyuz 15 Launch Vehicle: Soyuz 11A511. Apogee: 236 km (146 mi). Soyuz 15 was to conduct the second phase of manned operations aboard the Salyut 3 military space station, but the Igla rendezvous system failed and no docking was made. The two day flight could only be characterised as '... research in manoeuvring and docking with the OPS in various modes, and development of methods for evacuation and landing from space complex in new conditions....'
As Chelomei had complained, Soyuz had no reserves or backup systems for repeated manual docking attempts and had to be recovered after a two-day flight. The state commission found that the Igla docking system of the Soyuz needed serious modification. This could not be completed before Salyut 3 decayed. Therefore the planned Soyuz 16 spacecraft became excess to the program (it was later flown as Soyuz 20 to a civilian Salyut station, even though over its two year rated storage life). Officially: Conduct of joint experiments with the Salyut-3 orbital scientific station.
- 1974 December 2 09:40 - Soyuz 16 Launch Vehicle: Soyuz 11A511U. Apogee: 291 km (180 mi). ASTP Manned Test Flight. Check-out of the Soyuz space craft's on-board systems which had been modernized to meet the requirements of the 1975 joint flight in accordance with the programme of the Soviet-United States experiment; conduct of scientific and technical investigations.
- 1975 January 10 21:43 - Soyuz 17 Launch Vehicle: Soyuz 11A511. Apogee: 249 km (154 mi). Manned two crew. Docked with Salyut 4. Joint experiments with the Salyut scientific orbital station.
- 1975 April 5 11:04 - Soyuz 18-1 Launch Vehicle: Soyuz 11A511. During second-third stage seperation third stage failed to separate from second stage but still ignited.. Apogee: 192 km (119 mi). Carried Oleg Makarov, Vasili Lazarev for rendezvous with Salyut 4; but during second-third stage seperation third stage failed to separate from second stage but still ignited. The crew demanded that the abort procedures be implemented but ground control could not see the launch vehicle gyrations in their telemetry. Soyuz finally was separated from by ground control command at 192 km, and following a 20.6+ G reentry, the capsule landed in the Altai mountains, tumbled down a mountainside, and snagged in some bushes just short of a precipice. The crew was worried that they may have landed in China and would face internment, but after an hour sitting in the cold next to the capsule, they were discovered by locals speaking Russian. Total flight duration was 1574 km and flight time 21 minutes 27 seconds. Lazarev suffered internal injuries from the high-G reentry and tumble down the mountain side and never flew again. Both cosmonauts were denied their 3000 ruble spaceflight bonus pay and had to apeal all the way to Brezhnev before being paid.
- 1975 May 24 14:58 - Soyuz 18 Launch Vehicle: Soyuz 11A511. Apogee: 230 km (140 mi). Manned two crew. Docked with Salyut 4. Joint experiments with the Salyut scientific orbital station. The crew remained aloft aboard the station during the Apollo-Soyuz Test Project joint flight.
- 1975 July 15 12:20 - Soyuz 19 (ASTP) Launch Vehicle: Soyuz 11A511U. Apogee: 220 km (130 mi). Soyuz 19 initial orbital parameters were 220.8 by 185.07 kilometres, at the desired inclination of 51.80°, while the period of the first orbit was 88.6 minutes. On 17 July the two spacecraft docked. The crew members rotated between the two spacecraft and conducted various mainly ceremonial activities. Leonov was on the American side for 5 hours, 43 minutes, while Kubasov spent 4:57 in the command and docking modules.
After being docked for nearly 44 hours, Apollo and Soyuz parted for the first time and were station-keeping at a range of 50 meters. The Apollo crew placed its craft between Soyuz and the sun so that the diameter of the service module formed a disk which blocked out the sun. After this experiment Apollo moved towards Soyuz for the second docking.
Three hours later Apollo and Soyuz undocked for the second and final time. The spacecraft moved to a 40 m station-keeping distance so that an ultraviolet absorption experiment could be performed.
With all the joint flight activities completed, the ships went on their separate ways.
- 1975 September 29 04:15 - Cosmos 772 Launch Vehicle: Soyuz 11A511U. Apogee: 245 km (152 mi). Unmanned military Soyuz 7K-S test flight. Recovered October 3, 1975 4:10 GMT. Unsuccessful mission. Transmitted only on 166 MHz frequency, at none of the other usual Soyuz wavelengths.
Maneuver Summary: 193 km X 270 km orbit to 195 km X 300 km orbit. Delta V: 8 m/s 196 km X 300 km orbit to 196 km X 328 km orbit. Delta V: 8 m/s Total Delta V: 16 m/s
- 1975 November 17 14:36 - Soyuz 20 Launch Vehicle: Soyuz 11A511U. Apogee: 251 km (155 mi). Unmanned long duration test of the Soyuz transport vehicle; docked with Salyut 4. Recovered February 16, 1976 2:24 GMT. Comprehensive checking of improved on-board systems of the space craft under various flight conditions. Carried a biological payload. Living organisms were exposed to three months in space.
- 1976 July 6 12:08 - Soyuz 21 Launch Vehicle: Soyuz 11A511U. Apogee: 274 km (170 mi). Soyuz 21 with Volynov and Zholobov aboard hard-docked with the station on 6 July 1976 after failure of the Igla system at the last stage of rendezvous. Towards the end of the two month mission an early return to earth was requested due to the poor condition of flight engineer Zholobov (who was suffering from space sickness and psychological problems).
- 1976 September 15 09:48 - Soyuz 22 Launch Vehicle: Soyuz 11A511U. Apogee: 296 km (183 mi). Surplus Soyuz ASTP spacecraft modified with a multi-spectral camera manufactured by Carl Zeiss-Jena in place of the universal docking apparatus. Eight days were spent photographing the earth. Tested and perfected scientific-technical methods and devices for studying the geological characteristics of the earth's surface from outer space for economic purposes.
- 1976 October 14 17:39 - Soyuz 23 Launch Vehicle: Soyuz 11A511U. Apogee: 269 km (167 mi). The Soyuz 23 ferry spacecraft suffered a docking system failure. Sensors indicated an incorrect lateral velocity, causing unnecessary firing of the thrusters during rendezvous. The automatic system was turned off, but no fuel remained for a manual docking by the crew.
- 1976 November 29 16:00 - Cosmos 869 Launch Vehicle: Soyuz 11A511U. Apogee: 289 km (179 mi). Unmanned military Soyuz 7K-S test flight. Recovered December 17, 1976 10:31 GMT. Transmitted only on 20.008 MHz and 166 MHz frequencies, at none of the other usual Soyuz wavelengths.
Maneuver Summary: 196 km X 290 km orbit to 187 km X 335 km orbit. Delta V: 15 m/s 187 km X 335 km orbit to 259 km X 335 km orbit. Delta V: 21 m/s 259 km X 335 km orbit to 260 km X 345 km orbit. Delta V: 2 m/s 260 km X 345 km orbit to 265 km X 368 km orbit. Delta V: 7 m/s 265 km X 368 km orbit to 267 km X 391 km orbit. Delta V: 6 m/s 267 km X 391 km orbit to 300 km X 310 km orbit. Delta V: 32 m/s Total Delta V: 83 m/s
- 1977 February 7 16:10 - Soyuz 24 Launch Vehicle: Soyuz 11A511U. Apogee: 264 km (164 mi). Soyuz 24 docked with Salyut 5 and brought repair equipment and equipment for a change of cabin atmosphere. This special apparatus was designed to allow the entire station to be vented through the EVA airlock. Because of this the planned EVA was cancelled. However analysis after arrival showed no toxins in the air. The crew changed the cabin air anyway, then returned to earth. The mission, although a short 18 days, was characterised as a busy and successful mission, accomplishing nearly as much as the earlier Soyuz 21's 50 day mission.
- 1977 October 9 02:40 - Soyuz 25 Launch Vehicle: Soyuz 11A511U. Apogee: 240 km (140 mi). Manned two crew. Unsuccessful mission. Failed to dock with Salyut 6.
- 1977 December 10 01:18 - Soyuz 26 Launch Vehicle: Soyuz 11A511U. Apogee: 235 km (146 mi). Manned two crew. Docked with Salyut 6. Carried Yuri Romanenko, Georgi Grechko to Salyut 6; returned crew of Soyuz 27 to Earth. Conduct of joint experiments with the Salyut-6 scientific station.
- 1978 January 10 12:26 - Soyuz 27 Launch Vehicle: Soyuz 11A511U. Apogee: 237 km (147 mi). Manned two crew. Carried Oleg Makarov, Vladimir Dzhanibekov to Salyut 6; returned crew of Soyuz 26 to Earth. Docked with Salyut 6.
- 1978 March 2 15:28 - Soyuz 28 Launch Vehicle: Soyuz 11A511U. Apogee: 246 km (152 mi). Manned two crew. Docked with Salyut 6. Delivery to the Salyut-6 station of the first international 'Intercosmos' team consisting of A.A. Gubarev (USSR) and V. Remek (Czechoslovak Socialist Republic) to carry out scientific research and experiments jointly developed by Soviet a nd Czechoslovak specialists.
- 1978 April 4 15:00 - Cosmos 1001 Launch Vehicle: Soyuz 11A511U. Apogee: 228 km (141 mi). Manned precursor. Recovered April 15, 1978 12:02 GMT. Unsuccessful mission. Soyuz T test -failure.
Maneuver Summary: 202 km X 231 km orbit to 195 km X 291 km orbit. Delta V: 19 m/s 195 km X 291 km orbit to 306 km X 322 km orbit. Delta V: 40 m/s 306 km X 322 km orbit to 308 km X 318 km orbit. Delta V: 1 m/s Total Delta V: 60 m/s. Officially: Investigation of the upper atmosphere and outer space.
- 1978 June 15 20:16 - Soyuz 29 Launch Vehicle: Soyuz 11A511U. Apogee: 248 km (154 mi). Manned two crew. Docked with Salyut 6. Placed on board the Salyut-6 station a crew consisting of V.V. Kovalenko and A.S. Ivanchenkov to conduct scientific and technological investigations and experiments.
- 1978 June 27 15:27 - Soyuz 30 Launch Vehicle: Soyuz 11A511U. Apogee: 244 km (151 mi). Manned two crew. Docked with Salyut 6. Placed on board the Salyut-6 station, under the Intercosmos programme, a second, international, crew consisting of P.I. Klimuk (USSR) and M. Hermaszewski (Poland) to conduct scientific investigations and experiments.
- 1978 August 26 14:51 - Soyuz 31 Launch Vehicle: Soyuz 11A511U. Apogee: 243 km (150 mi). Manned two crew. Docked with Salyut 6. Delivered to the Salyut-6 station the third international 'Intercosmos' crew consisting of V F Bykovsky (USSR) and S Jaehn (German Democratic Republic) to carry out scientific research and experiments.
- 1978 October 3 23:09 - Progress 4 Launch Vehicle: Soyuz 11A511U. Soyuz 11A511U Ye15000-152 Apogee: 247 km (153 mi). Unmanned supply vessel to Salyut 6. Delivery of fuel, consumable materials and equipment to the Salyut 6 station. Docked with Salyut 6 on 6 Oct 1978 01:00:15 GMT. Undocked on 24 Oct 1978 13:01:52 GMT. Destroyed in reentry on 26 Oct 1978 16:28:13 GMT. Total free-flight time 4.22 days. Total docked time 18.50 days.
- 1980 April 27 06:24 - Progress 9 Launch Vehicle: Soyuz 11A511U. Soyuz 11A511U Zh15000-210 Apogee: 255 km (158 mi). Unmanned supply vessel for Salyut 6. Delivery of various cargoes to the Salyut-6 orbital station. Docked with Salyut 6 on 29 Apr 1980 08:09:19 GMT. Undocked on 20 May 1980 18:51:00 GMT. Destroyed in reentry on 22 May 1980 00:44:00 GMT. Total free-flight time 3.32 days. Total docked time 21.45 days.
- 1980 June 5 14:19 - Soyuz T-2 Launch Vehicle: Soyuz 11A511U. Apogee: 232 km (144 mi). Test flight of new Soyuz T; docked with Salyut 6. Conducted testing and development of on-board systems in the improved Soyuz T series transport vehicle under piloted conditions.
- 1980 June 29 04:40 - Progress 10 Launch Vehicle: Soyuz 11A511U. Soyuz 11A511U P15000-232 Apogee: 264 km (164 mi). Unmanned supply vessel for Salyut 6. Delivery of various cargoes to the Salyut-6 orbital station. Docked with Salyut 6 on 1 Jul 1980 05:53:00 GMT. Undocked on 17 Jul 1980 22:21:00 GMT. Destroyed in reentry on 19 Jul 1980 01:47:00 GMT. Total free-flight time 3.19 days. Total docked time 16.69 days.
- 1980 July 23 18:33 - Soyuz 37 Launch Vehicle: Soyuz 11A511U. Apogee: 273 km (169 mi). Manned two crew. Transported to the Salyut-6 station the sixth international crew under the Intercosmos programme, comprising V V Gorbatko (USSR) and Pham Tuan (Viet Nam), to conduct scientific research and experiments. Returned crew of Soyuz 35 to Earth. Recovered October 11, 1980 9:50 GMT.
- 1980 September 18 19:11 - Soyuz 38 Launch Vehicle: Soyuz 11A511U. Apogee: 257 km (159 mi). Manned two crew. Docked with Salyut 6. Transported to the Salyut-6 station the seventh international crew under the INTERCOSMOS programme, comprising Y V Romanenko (USSR) and A. Tomaio Mendez (Cuba), to conduct scientific research and experiments.
- 1980 September 28 15:09 - Progress 11 Launch Vehicle: Soyuz 11A511U. Soyuz 11A511U P15000-219 Apogee: 241 km (149 mi). Unmanned supply vessel for Salyut 6. Delivery of various cargoes to the Salyut-6 orbital station. Docked with Salyut 6 on 30 Sep 1980 17:03:00 GMT. Undocked on 9 Dec 1980 10:23:00 GMT. Destroyed in reentry on 11 Dec 1980 14:00:00 GMT. Total free-flight time 4.23 days. Total docked time 69.72 days.
- 1980 November 27 14:18 - Soyuz T-3 Launch Vehicle: Soyuz 11A511U. Apogee: 260 km (160 mi). Manned three crew. Docked with Salyut 6. Tested the improved transport ship of the 'SOYUZ T' series; transported to the Salyut-6 orbital station a crew consisting of L D Kizim, O G Makarov and G M Strekalov to carry out repair and preventive work and scientific and technical investigation and experiments.
- 1981 January 24 14:18 - Progress 12 Launch Vehicle: Soyuz 11A511U. Soyuz 11A511U P15000-235 Apogee: 308 km (191 mi). Unmanned supply vessel to Salyut 6. Delivery of various cargoes to the Salyut-6 orbital station. Docked with Salyut 6 on 26 Jan 1981 15:56:00 GMT. Undocked on 19 Mar 1981 18:14:00 GMT. Destroyed in reentry on 20 Mar 1981 16:59:00 GMT. Total free-flight time 3.02 days. Total docked time 52.10 days.
- 1981 March 12 19:00 - Soyuz T-4 Launch Vehicle: Soyuz 11A511U. Apogee: 237 km (147 mi). Manned two crew. Docked with Salyut 6. Transported to the Salyut-6 orbital station cosmonauts V V Kovalenok and V P Savinykh to carry out repairs and preventive maintenance and scientific and technical investigations and experiments.
- 1981 May 14 17:16 - Soyuz 40 Launch Vehicle: Soyuz 11A511U. Apogee: 270 km (160 mi). Manned two crew. Docked with Salyut 6. Transported to the Salyut-6 orbital station the ninth international crew under the INTERCOSMOS programme, comprising L I Popov (USSR), and D. Prunariu (Romania), to conduct scientific research and experiments.
- 1981 August 21 10:20 - Cosmos 1298 Launch Vehicle: Soyuz 11A511U. Apogee: 328 km (203 mi). High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission.
- 1982 April 2 10:15 - Cosmos 1347 Launch Vehicle: Soyuz 11A511U. Apogee: 337 km (209 mi). High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission.
- 1982 May 13 09:58 - Soyuz T-5 Launch Vehicle: Soyuz 11A511U. Apogee: 231 km (143 mi). Carried Anatoli Berezovoi, Valentin Lebedev to Salyut 7 to conduct scientific research and experiments; returned crew of Soyuz T-7 to Earth.
- 1982 May 23 05:58 - Progress 13 Launch Vehicle: Soyuz 11A511U. Soyuz 11A511U Ts15000-283 Apogee: 263 km (163 mi). Unmanned supply vessel to Salyut 7. Transport of various cargoes to the Salyut-7 orbital station. Docked with Salyut 7 on 25 May 1982 07:56:36 GMT. Undocked on 4 Jun 1982 06:31:00 GMT. Destroyed in reentry on 6 Jun 1982 00:05:00 GMT. Total free-flight time 3.81 days. Total docked time 9.94 days.
- 1982 June 12 - Yantar-4K1 Launch Vehicle: Soyuz 11A511U. Failure. High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission.
- 1982 June 24 16:29 - Soyuz T-6 Launch Vehicle: Soyuz 11A511U. Apogee: 233 km (144 mi). Manned three crew. Docked with Salyut 7. Transported to the Salyut-7 orbital station the Soviet-French international crew, comprising V A Dzhanibekov (USSR), A S Ivanchenkov (USSR) and Jean-Loup Chretien (France) to conduct scientific research and experiments.
- 1982 July 10 09:57 - Progress 14 Launch Vehicle: Soyuz 11A511U. Soyuz 11A511U Shch15000-318 Apogee: 325 km (201 mi). Unmanned supply vessel to Salyut 7. Docked with Salyut 7 on 12 Jul 1982 11:41:00 GMT. Undocked on 10 Aug 1982 22:11:00 GMT. Destroyed in reentry on 13 Aug 1982 01:29:00 GMT. Total free-flight time 4.21 days. Total docked time 29.44 days.
- 1982 August 19 17:11 - Soyuz T-7 Launch Vehicle: Soyuz 11A511U. Apogee: 299 km (185 mi). Docked with Salyut 7. Carried Svetlana Savitskaya, Leonid Popov, Alexander Serebrov to Salyut 7 to conduct scientific and technical research and experiments.
- 1982 September 18 04:58 - Progress 15 Launch Vehicle: Soyuz 11A511U. Soyuz 11A511U Ts15000-292 Apogee: 241 km (149 mi). Unmanned supply vessel to Salyut 7. Docked with Salyut 7 on 20 Sep 1982 06:12:00 GMT. Undocked on 14 Oct 1982 13:46:00 GMT. Destroyed in reentry on 16 Oct 1982 17:08:00 GMT. Total free-flight time 4.19 days. Total docked time 24.32 days.
- 1982 October 31 11:20 - Progress 16 Launch Vehicle: Soyuz 11A511U. Soyuz 11A511U Shch15000-335 Apogee: 246 km (152 mi). Unmanned supply vessel to Salyut 7. Docked with Salyut 7 on 2 Nov 1982 13:22:00 GMT. Undocked on 13 Dec 1982 15:32:00 GMT. Destroyed in reentry on 14 Dec 1982 17:17:00 GMT. Total free-flight time 3.16 days. Total docked time 41.09 days.
- 1982 December 8 13:46 - Cosmos 1423 Launch Vehicle: Molniya 8K78M. Fourth stage failure.. Apogee: 571 km (354 mi). Intended to replace Molniya 1-48; failed. Investigation of the upper atmosphere and outer space.
- 1983 April 20 13:10 - Soyuz T-8 Launch Vehicle: Soyuz 11A511U. Soyuz 11A511U 372 Apogee: 213 km (132 mi). Manned three crew. Unsuccessful mission. Failed to rendezvous with Salyut 7. Recovered April 22, 1983 13:29 GMT. Landed 113 km SE Arkalyk.
- 1983 June 27 09:12 - Soyuz T-9 Launch Vehicle: Soyuz 11A511U. Soyuz 11A511U 379 Apogee: 228 km (141 mi). Manned two crew. Docked with Salyut 7. Transported to the Salyut-7 orbital station a crew consisting of V A Lyakhov, commander of the spacecraft, and A P Aleksandrov, flight engineer, to conduct scientific and technical research and experiments.
- 1983 August 17 12:08 - Progress 17 Launch Vehicle: Soyuz 11A511U. Soyuz 11A511U Ts15000-302 Apogee: 242 km (150 mi). Unmanned supply vessel to Salyut 7. Docked with Salyut 7 on 19 Aug 1983 13:47:00 GMT. Undocked on 17 Sep 1983 11:44:00 GMT. Destroyed in reentry on 17 Sep 1983 23:43:00 GMT. Total free-flight time 2.57 days. Total docked time 28.91 days.
- 1983 September 26 19:37 - Soyuz T-10-1 Launch Vehicle: Soyuz 11A511U. Launch vehicle blew up on pad.. Apogee: 2.00 km (1.20 mi). Aborted September 27, 1983 19:38 GMT. Unsuccessful mission. Launch vehicle blew up on pad at Tyuratam; crew saved by abort system.
- 1984 August 14 06:28 - Progress 23 Launch Vehicle: Soyuz 11A511U. Soyuz 11A511U 711 Apogee: 250 km (150 mi). Transport of various cargoes to the Salyut-7 orbital station. Docked with Salyut 7 on 16 Aug 1984 08:11:00 GMT. Undocked on 26 Aug 1984 16:13:00 GMT. Destroyed in reentry on 28 Aug 1984 01:28:00 GMT. Total free-flight time 3.46 days. Total docked time 10.33 days.
- 1985 June 6 06:39 - Soyuz T-13 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 002 Apogee: 222 km (137 mi). Docked with Salyut 7. Delivered to the Salyut-7 orbital station a crew consisting of flight commander V A Dzhanibekov and flight engineer V P Savinykh to carry out emergency repairs to inert Salyut 7 station and to conduct scientific and technical research and experiments.
- 1985 June 21 00:39 - Progress 24 Launch Vehicle: Soyuz 11A511U. Soyuz 11A511U 417 Apogee: 251 km (155 mi). Delivery to the Salyut-7 orbital station of a mixed cargo with a total mass of 2,000 kg. Docked with Salyut 7 on 23 Jun 1985 02:54:00 GMT. Undocked on 15 Jul 1985 12:28:00 GMT. Destroyed in reentry on 15 Jul 1985 22:33:31 GMT. Total free-flight time 2.51 days. Total docked time 22.40 days.
- 1985 July 19 13:05 - Cosmos 1669 Launch Vehicle: Soyuz 11A511U. Soyuz 11A511U 446 Apogee: 247 km (153 mi). Progress vehicle, given Cosmos designation instead of Progress because control lost early in mission but regained later. Resupplied Salyut 7. On departure briefly undocked and redocked to verify reliability of docking system. Transported of various cargoes to the Salyut-7 orbital station. Docked with Salyut 7 on 21 Jul 1985 15:05:00 GMT. Undocked on 28 Aug 1985 21:50:00 GMT. Destroyed in reentry on 30 Aug 1985 01:20:00 GMT. Total free-flight time 3.23 days. Total docked time 38.28 days.
- 1985 September 17 12:38 - Soyuz T-14 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 007 Apogee: 223 km (138 mi). Docked with Salyut 7. Transported a crew comprising ship's commander V V Vasyutin, flight engineer G M Grechko and cosmonaut-researcher A A Volkov to the Salyut-7 orbital station to conduct scientific and technical studies and experiments. Grechko returned in Soyuz T-13 on 25 September 1985 - emergency return.
- 1986 March 13 12:33 - Soyuz T-15 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 012 Apogee: 366 km (227 mi). Mir Main Expedition EO-01. Epic repair mission. The crew, consisting of ship's commander L D Kizim and flight engineer V A Solovyov first docked with the Mir orbital station to conduct scientific and technical studies and experiments. Mir then maneuvered 17 April to match Salyut 7's orbit at 4000 km separation, then again on 4 May to catch up. After six weeks aboard Mir, Soyuz T-15 undocked on 5 May, then rendezvoused and manually docked with the inoperative Salyut 7 station. This was the only flight in history by a single spacecraft between two space stations. The Salyut-7 station was found to be ice bound and without electrical power. The crew repaired the station, regaining power, heat, and environmental control. The also removed experimental results left behind by last crew. Soyuz T-15 undocked Salyut 7 on 25 June, and redocked with Mir on 26 June, delivering 400 kg of scientific material from Salyut 7, including a multichannel spectrometer. Following further work aboard Mir, the crew landed on July 16, 1986 at 12:34 GMT. No crew ever revisited Salyut 7; it made an uncontrolled reentry over Argentina.
- 1986 March 19 10:08 - Progress 25 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 B15000-010 Apogee: 251 km (155 mi). Unmanned supply vessel transporting sundry cargoes to the Mir orbital station. Docked with Mir on 21 Mar 1986 11:16:02 GMT. Undocked on 20 Apr 1986 19:24:08 GMT. Destroyed in reentry on 21 Apr 1986 00:48:30 GMT. Total free-flight time 2.27 days. Total docked time 30.34 days.
- 1986 April 23 19:40 - Progress 26 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 B15000-009 Apogee: 257 km (159 mi). Unmanned supply vessel to Mir. Rendezvoused with Mir on 25 April, but problem with Mir's radio communication system delays docking until the next day. Docked with Mir on 26 Apr 1986 21:26:06 GMT. Undocked on 22 Jun 1986 18:25:00 GMT. Destroyed in reentry on 23 Jun 1986 15:41:01 GMT. Total free-flight time 3.96 days. Total docked time 56.87 days.
- 1986 May 21 08:21 - Soyuz TM-1 Launch Vehicle: Soyuz 11A511U2. Apogee: 225 km (139 mi). Test of new Soyuz vehicle. Recovered May 30, 1986 6:49 GMT. Unmanned test of Soyuz TM. Docked with Mir May 23 1987. Undocked 29 May.
Officially: Comprehensive experimental testing of spacecraft in independent flight and jointly with the Mir orbital station.
- 1987 January 16 06:06 - Progress 27 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 B15000-011 Apogee: 263 km (163 mi). Unmanned supply vessel to Mir; raised Mir's orbit. Transported sundry cargoes to the Mir orbital station. Docked with Salyut 7 on 18 Jan 1987 07:26:50 GMT. Undocked on 23 Feb 1987 11:29:01 GMT. Destroyed in reentry on 25 Feb 1987 16:05:00 GMT. Total free-flight time 4.25 days. Total docked time 36.17 days.
- 1987 February 5 21:38 - Soyuz TM-2 Launch Vehicle: Soyuz 11A511U2. Apogee: 365 km (226 mi). Mir Expedition EO-02. Docked with Mir 7 February 1987. Carried Yuri Romanenko, Aleksander Laveykin to Mir; returned Laveykin, crew of Soyuz TM-3 to Earth.
- 1987 March 3 11:14 - Progress 28 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 I15000-016 Apogee: 254 km (157 mi). Unmanned supply vessel to Mir. Orbit of station at time of rendezvous was 344 X 369 km, 51. 62 deg. Docked with Mir on 5 Mar 1987 12:42:36 GMT. Undocked on 26 Mar 1987 05:06:48 GMT. Destroyed in reentry on 28 Mar 1987 03:49:00 GMT. Total free-flight time 4.01 days. Total docked time 20.68 days.
- 1987 April 21 15:14 - Progress 29 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 I15000-015 Apogee: 237 km (147 mi). Unmanned supply vessel to Mir. Deorbited May 11, 1987. Docked with Mir at 343 X 363 1705 23 April at rear port of Kvant. Undocked May 11 03:10. Deorbited28 May 02:59 .
Officially: Transporting sundry cargoes to the Mir orbital station. Docked with Salyut 7 on 23 Apr 1987 17:04:51 GMT. Undocked on 11 May 1987 03:10:01 GMT. Destroyed in reentry on 11 May 1987 08:28:00 GMT. Total free-flight time 2.30 days. Total docked time 17.42 days.
- 1987 May 19 04:02 - Progress 30 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 I15000-018 Apogee: 365 km (226 mi). Unmanned supply vessel to Mir. Rendezvoused with Mir/Kvant in its orbit of 343 X 366 km, 51. 6 deg. Docked with the station on 21 May 1987 05:50:38 GMT. Undocked on 19 Jul 1987 00:19:51 GMT. Destroyed in reentry on 19 Jul 1987 05:42:00 GMT. Total free-flight time 2.30 days. Total docked time 58.77 days.
- 1987 July 22 01:59 - Soyuz TM-3 Launch Vehicle: Soyuz 11A511U2. Apogee: 353 km (219 mi). Manned three crew. Transported to the Mir orbital space station a Soviet-Syrian crew comprising cosmonauts A S Viktorenko, A P Aleksandrov and M A Faris to conduct joint research and experiments with cosmonauts Y Romanenko and A Laveykin. Maneuvered from initial 231 X 217 km orbit to Mir's 311 X 359 km orbit. Docked with rear Mir port at 3:30 GMT 24 July. Undocked with rear port 30 July and docked to forward port.
- 1987 August 3 20:44 - Progress 31 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 I15000-017 Apogee: 250 km (150 mi). Unmanned resupply vessel to Mir. Rendezvous transfer orbits 187 X 250 km, 51. 64 deg; 266 X 314 km; 309 X 360 km. Docked with Mir on 5 Aug 1987 22:27:35 GMT. Refueled Mir propellants tanks on 15/16 Sept. Undocked on 21 Sep 1987 23:57:41 GMT. Destroyed in reentry on 23 Sep 1987 01:02:00 GMT. Total free-flight time 3.12 days. Total docked time 47.06 days.
- 1987 September 23 23:43 - Progress 32 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 L15000-021 Apogee: 355 km (220 mi). Unmanned resupply vessel to Mir. Delivered 850 kg propellants, 315 kg food, 2,000 kg total. Docked with Mir on 26 Sep 1987 01:08:15 GMT. Undocked on 10 Nov 1987 04:09:10 GMT. Redocked from 2,500 m on 10 Nov 1987 05:47 GMT. Undocked again 17 Nov 1998 19:25 GMT. Destroyed in reentry on 19 Nov 1987 00:58:00 GMT. Total free-flight time 3.17 days. Total docked time 52.82 days.
- 1987 November 20 23:47 - Progress 33 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 L15000-022 Apogee: 343 km (213 mi). Unmanned resupply vessel to Mir. Space station orbit at rendezvous was 326 km x 343 km. Docked on 23 Nov 1987 01:39:13 GMT. Undocked on 19 Dec 1987 08:15:46 GMT. Destroyed in reentry on 19 Dec 1987 13:37:00 GMT. Total free-flight time 2.30 days. Total docked time 26.28 days.
- 1987 December 21 11:18 - Soyuz TM-4 Launch Vehicle: Soyuz 11A511U2. Apogee: 357 km (221 mi). Mir Expedition EO-03. Carried Musa Manarov, Anatoly Levchenko, Vladimir Titov to Mir; returned crew of Soyuz TM-5 to Earth. Orbits 168 x 243 km, 255 x 296 km, 333 x 359 km. Docked with Mir 12:51 GMT 23 December. 30 December moved to forward port.
- 1988 January 20 22:51 - Progress 34 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 L15000-025 Apogee: 347 km (215 mi). Unmanned resupply vessel to Mir. Docked on 23 Jan 1988 00:09:09 GMT. Undocked on 4 Mar 1988 03:40:09 GMT. Destroyed in reentry on 4 Mar 1988 07:29:30 GMT. Total free-flight time 2.21 days. Total docked time 41.15 days.
- 1988 March 23 21:05 - Progress 35 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 L15000-026 Apogee: 262 km (162 mi). Unmanned resupply vessel to Mir. Docked on 25 Mar 1988 22:21:35 GMT. Undocked on 5 May 1988 01:36:03 GMT. Destroyed in reentry on 5 May 1988 06:56:19 GMT. Total free-flight time 2.28 days. Total docked time 40.14 days.
- 1988 May 13 00:30 - Progress 36 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 L15000-023 Apogee: 246 km (152 mi). Unmanned resupply vessel to Mir. Rendezvous transfer orbits 185x246 km, 51. 66 deg; 223x334 km; 331x357 km. Docked with Mir on 15 May 1988 02:13:26 GMT. Undocked on 5 Jun 1988 11:11:55 GMT. Destroyed in reentry on 5 Jun 1988 21:18:40 GMT. Total free-flight time 2.49 days. Total docked time 21.37 days.
- 1988 June 7 14:03 - Soyuz TM-5 Launch Vehicle: Soyuz 11A511U2. Apogee: 216 km (134 mi). Transported to the Mir orbital station a Soviet/Bulgarian crew comprising cosmonauts A Y Solovyev, V P Savinykh and A P Aleksandrov (Bulgaria) to conduct joint research and experiments with cosmonauts V G Titov and M K Manarov. Interim orbit 343 x 282 km. Maneuvered to Mir's 355 x 349 km orbit. Docked 15:57 GMT 9 June to Mir's aft port. Moved to forward port 18 June.
- 1988 July 18 21:13 - Progress 37 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 L15000-024 Apogee: 256 km (159 mi). Unmanned resupply vessel to Mir. Rendezvous transfer orbits 187x256 km, 51. 62 deg; 235 x 319 km; 343 x 347 km. Docked with Mir on 20 Jul 1988 22:33:40 GMT. Refuelling operations on 7,8, and 9 August 1998. Undocked on 12 Aug 1988 08:31:54 GMT. Destroyed in reentry on 12 Aug 1988 13:45:40 GMT. Total free-flight time 2.27 days. Total docked time 22.42 days.
- 1988 August 29 04:23 - Soyuz TM-6 Launch Vehicle: Soyuz 11A511U2. Apogee: 228 km (141 mi). Transported to the Mir orbital station a Soviet-Afghan crew comprising the cosmonauts V A Lyakhov, V V Polyakov and A A Momand (Afghanistan) to conduct joint research and experiments with the cosmonauts V G Titov and M K Manarov. Returned Manarov, Titov (Soyuz TM-4), Chretien (Soyuz TM-7) to Earth. Initial orbit 195 X 228 km at 51. 57 deg. Maneuvered to a 235 x 259 km orbit, then docked with Mir at 05:41 GMT on 31 August at its 339 x 366 km orbit. Moved from aft to forward port 8 Sept 88.
- 1988 September 9 23:33 - Progress 38 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 76048930 Apogee: 248 km (154 mi). Unmanned resupply vessel to Mir. During launch first test of Buran ejection seat was made during ascent to orbit. The K-36M.11F35 seat was installed in an 'experimental droppable compartment' installed in place of the Launch Escape Tower engine on top of the shroud. Rendezvous orbits 186 X 246 km, 51. 63 deg; 234 X 332 km, 337 X 363 km. Docked with Mir on 12 Sep 1988 01:22:28 GMT. Delivered 2,000 kg supplies including 300 kg of food. Refuelled Mir. Undocked on 23 Nov 1988 12:12:46 GMT. Destroyed in reentry on 23 Nov 1988 19:06:58 GMT. Total free-flight time 2.36 days. Total docked time 72.45 days.
- 1988 November 26 15:49 - Soyuz TM-7 Launch Vehicle: Soyuz 11A511U2. Apogee: 235 km (146 mi). Mir Expedition EO-04. Carried Alexander Volkov, Sergei Krikalev, Jean-Loup Chretien to Mir; returned Volkov, Krikalev to Earth. Initial Orbit: 194 X 235 km. Thereafter maneuvered to rendezvous orbit 256 X 291 km before docking with Mir in 337 X 369 km at 17:16 GMT 28 November.
- 1988 December 25 04:11 - Progress 39 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 Ye15000-029 Apogee: 238 km (147 mi). Unmanned resupply vessel to Mir. Made second test of Buran ejection seat during ascent to orbit. The K-36M.11F35 seat was installed in an 'experimental droppable compartment' installed in place of the Launch Escape Tower engine on top of the shroud. Rendezvous orbits 187 X 237 km, 51.63 deg; 236 X 338 km; 325 X 353 km at Mir. Delivered 1,300 kg cargo. Docked with Mir on 27 Dec 1988 05:35:10 GMT. Undocked on 7 Feb 1989 06:45:34 GMT. Destroyed in reentry on 7 Feb 1989 13:49:00 GMT. Total free-flight time 2.35 days. Total docked time 42.05 days.
- 1989 February 10 08:53 - Progress 40 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 Ye15000-032 Apogee: 244 km (151 mi). Unmanned resupply vessel to Mir. Conducted third test of Buran ejection seat during ascent to orbit. The K-36M.11F35 seat was installed in an 'experimental droppable compartment' installed in place of the Launch Escape Tower engine on top of the shroud. Docked with Mir on 12 Feb 1989 10:29:38 GMT. Undocked on 3 Mar 1989 01:45:52 GMT. Unfurled experimental space mirror petal structure on undocking. Destroyed in reentry on 5 Mar 1989 01:59:00 GMT. Total free-flight time 4.08 days. Total docked time 18.64 days.
- 1989 March 16 18:54 - Progress 41 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 T15000-034 Apogee: 243 km (150 mi). Unmanned resupply vessel to Mir. Conducted fourth test of Buran ejection seat during ascent to orbit. The K-36M.11F35 seat was installed in an 'experimental droppable compartment' installed in place of the Launch Escape Tower engine on top of the shroud. Delivered Bulgarian Spektr 256 spectrometer, power supplies for failed equipment. Docked with Mir on 18 Mar 1989 20:50:46 GMT. Between April 9 and 17 boosted Mir into a 373 X 416 km storage orbit after the decision was made to delay remanning the station. However these maneuvers resulted in the spacecraft running out of fuel. Undocked on 21 Apr 1989 01:46:15 GMT. Destroyed in uncontrolled decay of orbit on 25 Apr 1989 12:12:00 GMT. Total free-flight time 6.52 days. Total docked time 33.21 days.
- 1989 July 18 12:10 - Cosmos 2031 Launch Vehicle: Soyuz 11A511U2. Apogee: 264 km (164 mi). First launch of Orlets-1 long duration film return military reconnaissance satellite. After returning multiple film capsules, the spacecraft was deorbited.
- 1989 August 23 03:09 - Progress M-1 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 T15000-037 Apogee: 217 km (134 mi). Unmanned supply vehicle to Mir; first flight of new vehicle design. Tested on-board systems under different conditions and delivered expendable materials and sundry cargo to the Mir manned space station. Docked with Mir on 25 Aug 1989 05:19:02 GMT. Undocked on 1 Dec 1989 09:02:23 GMT. Destroyed in reentry on 1 Dec 1989 11:21:00 GMT. Total free-flight time 2.19 days. Total docked time 98.16 days.
- 1989 September 5 21:38 - Soyuz TM-8 Launch Vehicle: Soyuz 11A511U2. Apogee: 392 km (243 mi). Manned two crew. Mir Expedition EO-05. Docked with Mir 8 September. Transported to the Mir orbital station a team consisting of A S Viktorenko, commander of the spacecraft, and A A Serebrov, on-board engineer, to carry out scientific and technological research and experiments. Flight cost 80 million rubles. Expected return 25 million rubles net profit.
- 1989 December 20 03:30 - Progress M-2 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 T15000-039? Apogee: 392 km (243 mi). Unmanned resupply vessel to Mir; carried US microgravity payload. Delivered various cargoes to the Mir orbital station, including scientific apparatus produced in the United States of America and intended, pursuant to a commercial agreement, for the conduct of experiments on space biotechnology. Docked with Mir on 22 Dec 1989 05:41:21 GMT. Undocked on 9 Feb 1990 02:33:07 GMT. Destroyed in reentry on 9 Feb 1990 07:56:00 GMT. Total free-flight time 2.31 days. Total docked time 48.87 days.
- 1990 February 11 06:16 - Soyuz TM-9 Launch Vehicle: Soyuz 11A511U2. Apogee: 387 km (240 mi). Manned two crew. Mir Expedition EO-06. Docked with Mir. Transported to the Mir orbital station a crew comprising the cosmonauts A Y Solovyov and A N Balandin to conduct an extensive programme of geophysical and astrophysical research, experiments on biology and biotechnology and work on space materials science.
- 1990 February 28 23:10 - Progress M-3 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 T15000-040 Apogee: 218 km (135 mi). Unmanned resupply vessel to Mir. Docked with Mir on 3 Mar 1990 01:04:32 GMT. Undocked on 27 Apr 1990 20:24:43 GMT. Destroyed in reentry on 28 Apr 1990 00:52:00 GMT. Total free-flight time 2.26 days. Total docked time 55.81 days.
- 1990 May 5 20:44 - Progress 42 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 T15000-041 Apogee: 243 km (150 mi). Unmanned resupply vessel to Mir; last of original design Progress spacecraft. Conducted fifth and final test of Buran ejection seat during ascent to orbit. The K-36M.11F35 seat was installed in an 'experimental droppable compartment' installed in place of the Launch Escape Tower engine on top of the shroud. Docked with Mir on 7 May 1990 22:45:03 GMT. Undocked on 27 May 1990 07:08:58 GMT. Destroyed in reentry on 27 May 1990 12:27:30 GMT. Total free-flight time 2.31 days. Total docked time 19.35 days.
- 1990 July 11 10:00 - Gamma Launch Vehicle: Soyuz 11A511U2. Apogee: 387 km (240 mi). Spacecraft mission was research in the field of high-energy (gamma/x-ray) astrophysics conducted jointly with France and Poland. The satellite was based on the Soyuz manned spacecraft and had an extremely long gestation - conceived in 1965, authorised in 1976, scheduled originally for launch in 1984, but further severe technical delays resulted in a 1990 launch.
- 1990 August 1 09:32 - Soyuz TM-10 Launch Vehicle: Soyuz 11A511U2. Apogee: 219 km (136 mi). Manned two crew. Docked with Mir. Mir Expedition EO-07. Transported to the Mir manned orbital station the crew consisting of the cosmonauts G M Manakov and G M Strekalov for the purpose of carrying out a programme of geophysical and astrophysical research, biological and biotechnological experiments, and work on space-materials science.
- 1990 August 15 04:00 - Progress M-4 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 T15000-042 Apogee: 219 km (136 mi). Unmanned resupply vessel to Mir. Delivered cables for rewiring operations and equipment for Soyuz TM-11 Japanese journalist flight. Docked with Mir on 17 Aug 1990 05:26:13 GMT. Undocked on 17 Sep 1990 12:42:43 GMT. Destroyed in reentry on 20 Sep 1990 11:42:49 GMT. Total free-flight time 5.02 days. Total docked time 31.30 days.
- 1990 September 27 10:37 - Progress M-5 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 T15000-044 Apogee: 229 km (142 mi). Unmanned resupply vessel to Mir. Included first Progress recoverable capsule for return of 150 kg of payload to earth. Docked with Mir on 29 Sep 1990 12:26:50 GMT. Undocked on 28 Nov 1990 06:15:46 GMT. After deorbit burn, capsule separated for reentry with an expected landing in Kazakhstan at 28 Nov 1990 11:04:05 GMT. However the recoverable capsule's beacon signal was never received after reentry. All experimental data and materials in capsule lost. Total free-flight time 2.28 days. Total docked time 59.74 days.
- 1990 October 1 11:00 - Cosmos 2101 Launch Vehicle: Soyuz 11A511U2. Apogee: 304 km (188 mi). Long duration film return military reconnaissance satellite. After returning multiple film capsules, the spacecraft was deorbited.
- 1990 December 2 08:13 - Soyuz TM-11 Launch Vehicle: Soyuz 11A511U2. Apogee: 400 km (240 mi). Docked with Mir. Mir Expedition EO-08. Transported to the Mir manned orbital station the international crew consisting of the cosmonauts V M Afanasyev, M Kh Manarov, and T Akiyami (Japan) for the purpose of carrying out joint work with the cosmonauts G M Manakov and G M Strekalov. Launched jointly with the private Japanese company TBS. The Japanese television network ended up paying $ 28 million for the first commercial flight to Mir to put Akiyama, the first journalist in space aboard Soyuz TM-11. Akiyama made daily television broadcasts.
- 1991 January 14 14:50 - Progress M-6 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 T15000-045 Apogee: 205 km (127 mi). Unmanned resupply vessel to Mir. Delivered new life support equipment to replace life-expired equipment aboard. Docked with Mir on 16 Jan 1991 16:35:25 GMT. Undocked on 15 Mar 1991 12:46:41 GMT. Destroyed in reentry on 15 Mar 1991 18:07:26 GMT. Total free-flight time 2.30 days. Total docked time 57.84 days.
- 1991 February 15 09:30 - Cosmos 2134 Launch Vehicle: Soyuz 11A511U. Apogee: 306 km (190 mi). Topographic mapping for the Army General Staff.
- 1991 March 19 13:05 - Progress M-7 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 R15000-049 Apogee: 213 km (132 mi). Unmanned resupply vessel to Mir. Attempted to dock with Mir on 21 March 1998 14:28 GMT, but missed the station by 500 m. Docking attempted again on 23 March but at 50 meters the docking was aborted; the Progress missed hitting the station by five meters. Thereafter it was placed in a station-keeping co-orbit with Mir while the problem was diagnosed. Finally docked with Mir on 28 Mar 1991 12:02:28 GMT. On 12 and 14 Apr 1998 two burns of the engine of Progress M-7 raised the station's orbit from a 360 x 377 km orbit to a 370 x 382 km orbit. Undocked on 6 May 1991 22:59:36 GMT. Destroyed in reentry on 7 May 1991 17:20:05 GMT. Total free-flight time 9.72 days. Total docked time 39.46 days.
- 1991 May 18 12:50 - Soyuz TM-12 Launch Vehicle: Soyuz 11A511U2. Apogee: 397 km (246 mi). Docked with Mir. Mir Expedition EO-09. Carried Anatoli Artsebarski, Sergei Krikalev, Helen Sharman to Mir; returned Artsebarski, crew of Soyuz TM 8 to Earth. Second commercial flight with paying British passenger. Sponsoring British consortium was not quite able to come up with money, however. Flight continued at Soviet expense with very limited UK experiments.
- 1991 May 30 08:04 - Progress M-8 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 R15000-050 Apogee: 396 km (246 mi). Unmanned resupply vessel to Mir. Docked with Mir on 1 Jun 1991 09:44:37 GMT. Undocked on 15 Aug 1991 22:16:59 GMT. Destroyed in reentry on 16 Aug 1991 06:56:32 GMT. Total free-flight time 2.43 days. Total docked time 75.52 days.
- 1991 August 20 22:54 - Progress M-9 Launch Vehicle: Soyuz 11A511U2. Soyuz 11A511U2 G15000-047 Apogee: 230 km (140 mi). Unmanned resupply vessel to Mir; carried reentry capsule for return of 150 kg of experiment results. Docked with Mir on 23 Aug 1991 00:54:17 GMT. Undocked on 30 Sep 1991 01:53:00 GMT. 350 kg return capsule detached from the Propess' orbital module at an altitude of 110 to 130 km. The capsule underwent a ballistic descent to 15 km, followed by a parachute descent from there to surface. The capsule's beacon began transmitting at 4.5 km. Landed in Kazakhstan on 30 Sep 1991 08:16:24 GMT. Total free-flight time 2.35 days. Total docked time 38.04 days.
- 1991 October 2 05:59 - Soyuz TM-13 Launch Vehicle: Soyuz 11A511U2. Apogee: 232 km (144 mi). Manned three crew. Docked with Mir. Mir Expedition EO-10. Transported to the Mir manned orbital station an interna
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