Salyut 1

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Salyut 1 (DOS-1)
Reentry
October 11, 1971 (1971-10-12)
Mission statusDe-orbited
Mass18,425 kg (40,620 lb)
Length~20 m (66 ft)
Diameter~4 m (13 ft)
Pressurized volume99 m3 (3,500 cu ft)
Perigee altitude200 km (124 mi)
Apogee altitude222 km (138 mi)
Orbital inclination51.6 degrees
Orbital period88.5 minutes
Days in orbit175 days
Days occupied24 days
No. of orbits2,929
Distance traveled118,602,524 km (73,696,192 mi)
Configuration
Soyuz docking with Salyut 1

Salyut 1 (DOS-1) (

Salyut program followed this with five more successful launches of seven more stations. The final module of the program, Zvezda (DOS-8), became the core of the Russian segment of the International Space Station
and remains in orbit.

Salyut 1 was modified from one of the Almaz airframes, and was made out of five components: a transfer compartment, a main compartment, two auxiliary compartments, and the Orion 1 Space Observatory.

Salyut 1 was visited by Soyuz 10 and Soyuz 11. The hard-docking of Soyuz 10 failed and the crew had to abort this mission. The Soyuz 11 crew achieved successful hard docking and performed experiments in Salyut 1 for 23 days. However, they were killed by asphyxia caused by failure of a valve just prior to Earth reentry, and are the only people to have died above the Kármán line. Salyut 1's mission was later terminated, and it burned up on reentry into Earth's atmosphere on October 11, 1971.

Background

Salyut 1 originated as a modification of the Soviet military's Almaz space station program that was then in development.[2] After the landing of Apollo 11 on the Moon in July 1969, the Soviets began shifting the primary emphasis of their crewed space program to orbiting space stations, with a possible lunar landing later in the 1970s if the N-1 rocket became flight-worthy.[3] Leonid Brezhnev canceled the lunar landing program in 1974 after four catastrophic N-1 launch failures. One other motivation for the space station program was a desire to one-up the US Skylab program then in development. The basic structure of Salyut 1 was adapted from the Almaz with a few modifications and would form the basis of all Soviet space stations through Mir.[2]

Civilian Soviet space stations were internally referred to as DOS (the Russian acronym for "Long-duration orbital station"), although publicly, the Salyut name was used for the first six DOS stations (Mir was internally known as DOS-7).[2] Several military experiments were nonetheless carried on Salyut 1, including the OD-4 optical visual ranger,[4] the Orion ultraviolet instrument for characterizing rocket exhaust plumes,[5] and the highly classified Svinets radiometer.[6][self-published source]

Construction and operational history

Construction of Salyut 1 began in early 1970, and after nearly a year it was shipped to the Baikonur Cosmodrome. Some remaining assembly had yet to be done, and this was completed at the launch center. The Salyut programme was managed by Kerim Kerimov,[7] chairman of the state commission for Soyuz missions.[8]

Launch was planned for April 12, 1971 to coincide with the 10th anniversary of

de-orbiting after six months in orbit, because it ran out of fuel before a redesigned Soyuz spacecraft could be launched to it.[10]

Structure

At launch, the announced purpose of Salyut was to test the elements of the systems of a space station and to conduct scientific research and experiments. The craft was described as being 20 m (66 ft) in length, 4 m (13 ft) in maximum diameter, and 99 m3 (3,500 cu ft) in interior space with an on-orbit dry mass of 18,425 kg (40,620 lb). Of its several compartments, three were pressurized (100 m3 total), and two could be entered by the crew.[1]

Transfer compartment

The transfer compartment was equipped with the only docking port of Salyut 1, which allowed one Soyuz 7K-OKS spacecraft to dock. It was the first use of the Soviet SSVP docking system that allowed internal crew transfer, a system that is in use today. The docking cone had a 2 m (6.6 ft) front diameter and a 3 m (9.8 ft) aft diameter.[1]

Main compartment

The second and main compartment was about 4 m (13 ft) in diameter. Televised views showed enough space for eight large chairs (seven at work consoles), several control panels, and 20 portholes (some obstructed by instruments).[1] In Salyut 1 the interior design used various colors (light and dark gray, apple green, light yellow) for supporting the cosmonauts’ orientation in weightlessness.[11]

Auxiliary compartments

The third pressurized compartment contained the control and communications equipment, the power supply, the

life support system, and other auxiliary equipment. The fourth and final unpressurized compartment was about 2 m in diameter and contained the engine installations and associated control equipment. Salyut had buffer chemical batteries, reserve supplies of oxygen and water, and regeneration systems. Externally mounted were two double sets of solar cell panels that extended like wings from the smaller compartments at each end, the heat regulation system's radiators, and orientation and control devices.[1]

Salyut 1 was modified from one of the Almaz airframes. The unpressurized service module was the modified service module of a Soyuz craft.[2]

Orion 1 Space Observatory

The astrophysical

spectrograph of the Wadsworth system using film sensitive to the far ultraviolet. The dispersion of the spectrograph was 32 Å/mm (3.2 nm/mm), while the resolution of the spectrograms derived was about 5 Å at 2600 Å (0.5 nm at 260 nm). Slitless spectrograms were obtained of the stars Vega and Beta Centauri between 2000 and 3800 Å (200 and 380 nm).[12] The telescope was operated by crew member Viktor Patsayev, who became the first man to operate a telescope outside of the Earth's atmosphere.[13]

Specifications

Visiting spacecraft and crews

The only spacecraft that ever docked to Salyut 1 were Soyuz 10 and Soyuz 11. Soyuz 10 failed to hard-dock with Salyut 1 and had to abort the mission. Soyuz 11 conducted experiments in Salyut 1 for 23 days, however the cosmonauts later died during reentry in their Soyuz capsule.

Soyuz 10

Still frame from an animation of Salyut 1 with attached Soyuz.

Soyuz 10 was launched on April 22, 1971, carrying cosmonauts Vladimir Shatalov, Aleksei Yeliseyev, and Nikolai Rukavishnikov. After taking 24 hours for rendezvous and approach, Soyuz 10 soft-docked with Salyut 1 on April 24 at 01:47 UTC and remained for 5.5 h.[1] Hard-docking was unsuccessful due to technical malfunctions. The crew could not enter the station and had to return to Earth on April 24.[14]

Soyuz 11

The Soyuz 11 crew with the Salyut station in the background, in a Soviet commemorative stamp

Soyuz 11 was launched on June 6, 1971 at 04:55:09 UTC and took 3 hours and 19 minutes on June 7 to complete docking.[15] The cosmonauts Georgy Dobrovolsky, Viktor Patsayev, and Vladislav Volkov entered to Salyut 1 and their mission was announced as:[1]

  • Checking the design, units, onboard systems, and equipment of the orbital piloted station.
  • Testing the station's manual and autonomous procedures for orientation and navigation, as well as the control systems for maneuvering the space complex in orbit.
  • Studying Earth's surface geology, geography, meteorology, and snow and ice cover.
  • Studying physical characteristics, processes, and phenomena in the atmosphere and outer space in various regions of the electromagnetic spectrum.
  • Conducting medico-biological studies to determine the feasibility of having cosmonauts in the station perform various tasks, and studying the influence of space flight on the human organism.

On June 29, after 23 days and flying 362 orbits, the mission was cut short due to problems aboard the station, including an electrical fire. The crew transferred back to Soyuz 11 and reentered the Earth's atmosphere. The capsule parachuted to a soft landing at 23:16:52 UTC in Kazakhstan, but the recovery team opened the hatch to find all three crew members dead in their couches. An inquest found that a pressure relief valve had malfunctioned during reentry leading to a loss of cabin atmosphere.[16] The crew were not wearing pressure suits, and it was decreed by the TsKBEM (the team of engineers who investigated the tragedy) that all further Soyuz missions would require the use of them.[17]

Reentry of Salyut 1

Salyut 1 was moved to a higher orbit in July–August 1971 to ensure that it would not be destroyed prematurely through orbital decay. In the meantime, Soyuz capsules were being substantially redesigned to allow pressure suits to be worn during launch, docking maneuvers, and re-entry.[18] The Soyuz redesign effort took too long however, and by September, Salyut 1 was running out of fuel.[10] It was decided to conclude the station's mission and on October 11, the main engines were fired for a deorbit maneuver. After 175 days, the world's first space station burned up over the Pacific Ocean.[1]

Pravda (October 26, 1971) reported that 75% of Salyut 1's studies were carried out by optical means and 20% by radio-technical means, while the remainder involved magnetometrical, gravitational, or other measurements. Synoptic readings were taken in both the visible and invisible parts of the electromagnetic spectrum.[1]

See also

  • Salyut 6 – Former Soviet orbital space station
  • Soviet space program – Space exploration program conducted by the Soviet Union from 1955 to 1991

References

Citations

  1. ^ a b c d e f g h i "Salyut 1". NSSDC ID: 1971-032A. NASA. Retrieved March 24, 2012.
  2. ^ a b c d e Portree 1995.
  3. ^ Baker 2007, p. 18.
  4. ^ Ivanovich 2008, p. 9.
  5. ^ Ivanovich 2008, p. 29.
  6. ^ Oberg, James (December 18, 2016). "Have cosmonauts seen launches?" (PDF). p. 4. Retrieved April 18, 2018.
  7. ISBN 978-0-8032-2292-2
    .
  8. ^ Ivanovich 2008, p. 56.
  9. ISBN 9780030320163
    .
  10. ^ a b Shayler & Hall 2003, p. 179.
  11. OCLC 759926461
    .
  12. S2CID 4265702
    .
  13. ISBN 9781461468004
    . Retrieved April 18, 2018.
  14. ^ Shayler & Hall 2003, p. 174.
  15. ^ "Soyuz 11". NSSDC ID: 1971-035A. NASA. Retrieved March 24, 2012.
  16. ^ Baker 2007, pp. 23–25.
  17. ^ Shayler & Hall 2003, p. 180.
  18. ^ Baker 2007, p. 25.

Sources

External links
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