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Salyut Space Stations - Technical Details
Salyut Six
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Introduction

Salyut Six (DOS-5) was the eighth station of the Salyut programme and the fifth of the Durable Orbital Station series of civilian space stations. It was launched on 29 September 1977 by a Proton rocket and was the first space station to receive crewed and un-crewed spacecraft for human habitation, crew transfer, international participation and resupply. This established precedents for station life and operations on the later Mir and the International Space Stations.

Salyut Six was the first "second generation" soviet space station with major improvements in capabilities and operation. It had a new propulsion system and two docking ports, allowing two craft to visit simultaneously. This feature made it possible for crews to be re-supplied and remain aboard for several months.

Salyut Six with Soyuz T-4 docked
Salyut Six with Soyuz T-4 crew craft
[Click image to enlarge]

Six long-term resident crews were supported by ten short-term visiting crews who arrived in newer Soyuz craft and departed in older craft. This left the newer craft available to the resident crew as a return vehicle so that they could stay past the design life of a Soyuz craft. Short-term visiting crews routinely included international cosmonauts from Warsaw pact countries participating in the Soviet Union's Intercosmos programme. These cosmonauts were the first from countries other than the Soviet Union or the United States.

Salyut Six was re-supplied by twelve un-crewed Progress spacecraft starting with Progress 1, the first of the series. Also it saw the first operational use of the new Soyuz-T spacecraft.

From 1977 to 1981, the station was occupied by crews during six separate, discontinuous intervals. Between each of these intervals Salyut 6 was vacant, although it was visited by Soyuz T-1 and Kosmos 1267 on un-crewed test missions. Following the launch of Salyut Seven, Salyut Six was de-orbited and destroyed on 29 July 1982 after five years in orbit.

Reference: Wikipedia - Salyut 6

Research

The primary research instrument on Salyut Six was the BST-1M multispectral telescope, which could carry out astronomical observations in the infrared, ultraviolet and submillimeter spectra. It used a 1.5 metre-diameter mirror, which was operated in cryogenic conditions at around -269 °C (4 K). The telescope could be operated only when the station was on the night side of the Earth. Its cover was closed for the rest of the time.

The second major instrument was the MKF-6M multispectral camera, which carried out Earth-resources observations. This camera captured an area of 165 by 220 kilometres with each image, down to a resolution of 20 meters. Each image was captured simultaneously in six bands in 1200-frame cassettes. These required regular replacement due to the fogging effects of radiation.

Salyut Six also featured a KATE-140 stereoscopic topographic mapping camera with a focal length of 140 millimetres. This captured images of 450 by 450 kilometers with a resolution of 50 meters in the visible and infrared spectra. It could be operated either remotely or by the resident crews.

Salyut Six was also equipped with 20 portholes for observations, two scientific airlocks to expose equipment to space or eject rubbish, and various pieces of apparatus to carry out biological experiments. Later on during the flight, a Progress spacecraft delivered an external telescope, the KRT-10 [ru] radio observatory, which incorporated a directional antenna and five radiometers. The antenna was deployed on the rear docking assembly, with the controller remaining inside the station, and was used for both astronomical and meteorological observations.

Salyut Six, Soyuz & Progress
Salyut Six with Soyuz and Progress craft
[Click image to enlarge]

Design

Although the previous civilian stations carried out some research, they were mainly focused on testing and development. Salyut Six was the first station to become fully operational using the experience gained from the earlier stations. Its navigation system using the Delta semi-automatic computer, to depict the station's orbit, and the Kaskad system to control its orientation, was based on that used on Salyut Four. Its power system, consisting of a trio of steerable solar panels, and its thermal regulation systems was also based on those used on Salyut four. Salyut Six also used environmental systems and controlled its orientation using gyrodynes which were first used on Salyut Three.

Salyut Six's rear docking port was fitted with plumbing to allow the station to be refueled by un-crewed Progress spacecraft. These craft brought supplies and extra equipment to keep the station replenished, helped ensure that the crew were always able to carry out useful scientific work aboard the station. In all, twelve Progress flights delivered over 20 tonnes of equipment, supplies and fuel to the station.

Propulsion System

To allow for the rear docking port, Salyut Six used the Almaz-derived twin-chamber propulsion system first used on Salyut Three and Five. This had two engine nozzles, each producing 2.9 kilonewtons of thrust, mounted peripherally on either side of the port. This unified propulsion system had both the engines and the station's control thrusters running on unsymmetrical dimethylhydrazine and nitrogen tetroxide, drawn from a common set of pressurized tanks.

This resulted in more efficient refueling by the Progress craft. The entire engine and fuel storage assembly was located in an unpressurized bay at the rear of the station. This section had the same diameter as the main pressurized compartment. The main engines could not be fired if the rear docking port was in use so any orbital maneuvers during this time had to be performed by the visiting spacecraft.

Salyut 6 inside photo
Salyut 6 inside
[Click image to enlarge]

Salyut Six's propulsion system experienced a serious malfunction during the second crew residency in 1978 and was not usable again for the remainder of the station's lifespan. This meant that visiting spacecraft had to be used to perform orbital adjustments. After each crew residency ended, it was necessary for Progress and TKS spacecraft to boost the station into a high orbit so it would not decay before the next crew arrived.

Crew Facilities

Living conditions for the crews on Salyut Six were considerably improved over previous stations. Machinery was soundproofed, the crews were provided with designated "cots" for sleeping and the station had a shower and extensive gymnasium.

To enable spacewalks, Salyut Six was equipped with an inward-opening EVA hatch on the side of the forward transfer compartment, which could be used as an airlock similar to Salyut Four. This compartment contained two new semi-rigid spacesuits, which allowed much greater flexibility than earlier suits. They could be donned within five minutes in an emergency.

Statistics


Launch: September 29, 1977
Carrier rocket: Proton-K
Launch pad: Baikonur, Site 81/24
Re-entry: July 29, 1982
Perigee altitude: 219 km
Apogee altitude: 275 km
Orbital inclination: 51.6°
Orbital period: 89.1 minutes
Days in orbit: 1,764 days
Days occupied: 683 days
No. of orbits: 28,024

Specifications


Length: 15.8 m
Diameter: 4.15 m
Habitable volume: 90 m3
Mass at Launch: 19,824 kg
Major Ports: 2
Main engines: 2
Main engine power: 2.9 kN each

Salyut Six Expedition Two crew playing Chess
Salyut Six Expedition Two crew
[Click image to enlarge]

Expeditions and Missions

The table below gives a summary of the station crew (Expeditions), visiting crew and crew craft test missions to Salyut Six (DOS-5).

Expd
No.
 ℹ 

Expedition crew I.D.

Crew
No.
 ℹ 

Number of crew on mission

Launch Return Duration
(Days)
 ℹ 

Number of days in orbit

Mission Notes
 ℹ 

General notes on the mission

Year Date Spacecraft Year Date Spacecraft
- 2 1977 Nov 9 Soyuz 25 1977 Nov 11 Soyuz 25 2 Soyuz 25 failed to dock.
EO-1 2 Dec 10 Soyuz 26 1978 Mar 16 Soyuz 27 96 First operational crew on Salyut 6.
EP-1 2 1978 Jan 10 Soyuz 27 Jan 16 Soyuz 26 6 Replacement standby craft for EO-1 crew.
EP-2 2 Mar 2 Soyuz 28 Mar 10 Soyuz 28 8 Visiting crew with first non-Soviet (Czechoslovakian) cosmonaut.
EO-2 2 Jun 15 Soyuz 29 Nov 2 Soyuz 31 140 Second Expedition station crew.
EP-3 2 Jun 27 Soyuz 30 Jul 5 Soyuz 30 8 Visiting crew with non-Soviet (Polish) cosmonaut.
EP-4 2 Aug 26 Soyuz 31 Sep 31 Soyuz 29 8 Replacement standby craft for EO-2 crew.
EO-3 2 1979 Feb 25 Soyuz 32 1979 Aug 19 Soyuz 34 175 Third Expedition station crew. Soyuz 32 returned un-crewed.
- 2 Apr 10 Soyuz 33 Apr 12 Soyuz 33 2 Soyuz 33 engine fault. Failed to dock and returned to Earth.
- 0 Jun 6 Soyuz 34 Aug 19 Soyuz 34 65 Launched un-crewed as standby and return craft for EO-3 crew.
- 0 Dec 16 Soyuz T-1 1980 Mar 23 Soyuz T-1 95 Un-crewed test of the newly designed Soyuz T crewed craft.
EO-4 2 1980 Apr 9 Soyuz 35 Oct 11 Soyuz 37 185 Fourth Expedition station crew.
EP-5 2 May 26 Soyuz 36 Jun 3 Soyuz 35 8 Replacement standby craft for EO-4 crew.
EP-6 2 Jun 5 Soyuz T-2 Jun 9 Soyuz T-2 4 Crewed test of Soyuz T craft.
EP-7 2 Jul 23 Soyuz 37 Jul 31 Soyuz 36 8 Second replacement standby craft for EO-4 crew.
EP-8 2 Sep 18 Soyuz 38 Sep 26 Soyuz 38 8 Visiting crew with non-Soviet (Cuban) cosmonaut.
EO-5 3 Nov 27 Soyuz T-3 Dec 10 Soyuz T-3 12 Fifth Expedition station crew. First time with three crew.
EO-6 2 1981 Mar 12 Soyuz T-4 1981 May 26 Soyuz T-4 74 Sixth and last Expedition station crew on Salyut 6.
EP-9 2 Mar 22 Soyuz 39 Mar 30 Soyuz 39 8 Visiting crew with non-Soviet (Mongolian) cosmonaut.
- 0 Apr 25 Kosmos 1267 1982 Jul 29 Kosmos 1267 405 Un-crewed test of TKS scientific expansion module. Only re-entry capsule returned.
EP-10 2 May 14 Soyuz 40 1981 May 22 Soyuz 40 8 Visiting crew with non-Soviet (Romanian) cosmonaut.
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