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Salyut 4 (DOS 4) ( ; English translation: Salute 4) was a Salyut space station launched on December 26, 1974 into an orbit with an apogee of 355 km, a perigee of 343 km and an orbital inclination of 51.6 degrees. It was essentially a copy of the DOS 3, and unlike its ill-fated sibling it was a complete success. Three crews attempted to make stays aboard Salyut 4 (Soyuz 17 and Soyuz 18 docked; Soyuz 18a suffered a launch abort). The second stay was for 63 days duration, and an unmanned Soyuz capsule remained docked to the station for three months, proving the system's long-term durability. Salyut 4 was deorbited February 2, 1977, and re-entered the Earth's atmosphere on February 3.

Instrumentation

Installed on the Salyut 4 were OST-1 (Orbiting Solar Telescope) 25 cm solar telescope, designed at the Crimean Astrophysical Observatorymarker, and two X-ray telescopes. One of X-ray telescopes, often called the Filin telescope, consisted of four gas flow proportional counters, three of which had a total detection surface of 450 cm² in the energy range 2-10 keV, and one of which had an effective surface of 37 cm² for the range 0.2 to 2 keV (32 to 320 aJ). The field of view was limited by a slit collimator to 3 in × 10 in full width at half maximum. The instrumentation also included optical sensors which were mounted on the outside of the station together with the X-ray detectors, and power supply and measurement units which were inside the station. Ground based calibration of the detectors was considered along with in-flight operation in three modes: inertial orientation, orbital orientation, and survey. Data could be collected in 4 energy channels: 2 to 3.1 keV (320 to 497 aJ), 3.1 to 5.9 keV (497 to 945 aJ), 5.9 to 9.6 keV (945 to 1,538 aJ), and 2 to 9.6 keV (320 to 1,538 aJ) in the larger detectors. The smaller detector had discriminator levels set at 0.2 keV (32 aJ), 0.55 keV (88 aJ), and 0.95 keV (152 aJ).

Science

Among others, observations of Sco X-1, Cir X-1, Cyg X-1, and A0620-00 were published from the Filin data. A highly variable low energy of 0.6 to 0.9 keV (96 to 144 aJ) flux was detected in Sco X-1. Cir X-1 was not detected at all during a July 5, 1975 observation, providing an upper limit on the emission of 3.5e-11 erg·cm-2·s-1 (35 fW/m²) in the 0.2 to 2.0 keV (32 to 320 aJ) range. Cyg X-1 was observed on several occasions. Highly variable flux, in both the time and energy domains, was observed.

Specifications

  • Length - 15.8 m
  • Maximum diameter - 4.15 m
  • Habitable volume - 90 m³
  • Weight at launch - 18,900 kg
  • Launch vehicle - Proton (three-stage)
  • Orbital inclination - 51.6°
  • Area of solar arrays - 60 m²
  • Number of solar arrays - 3
  • Electricity production - 4 kW
  • Resupply carriers - Soyuz Ferry
  • Number of docking ports - 1
  • Total manned missions - 3
  • Total unmanned missions - 1
  • Total long-duration manned missions - 2


Visiting spacecraft and crews







  • Soyuz 20 - November 17, 1975 - February 16, 1976
    • no crew


Salyut 4 Expeditions

Expedition Crew Launch date Flight up Landing date Flight down Duration (days) Notes
Soyuz 17 Georgi Grechko,
Aleksei Gubarev
January 11, 1975
21:43:37 UTC
Soyuz 17 February 10, 1975
11:03:22 UTC
Soyuz 17 29.56 Launch from Baikonur; landing 110 km northeast of Tselinograd; docking on space station Salyut 4, which had been launched 3 days earlier; transfer into space station and 29 days stay time there; astronomical experiments.
Soyuz 18 Pyotr Klimuk,
Vitali Sevastyanov
May 24, 1975
14:58:10 UTC
Soyuz 18 July 26, 1975
14:18:18 UTC
Soyuz 18 62.97 Launch from Baikonur; landing 56 km east of Arkalyk; 2. crew of spacestation Salyut 4; 62 days staying time; intensive fitness training; breeding of "space vegetable"; solar observation; taking photographs of Earth surface.


See also



References

  1. Salyut 4
  2. The design of the Salyut-4 orbiting solar telescope






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