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The Salyut programme (, , meaning "salute" or "fireworks") was the first programme, undertaken by the . It involved a series of four crewed scientific research space stations and two crewed military reconnaissance space stations over a period of 15 years, from 1971 to 1986. Two other Salyut launches failed. In one respect, Salyut had the space-race task of carrying out long-term research into the problems of living in space and a variety of astronomical, biological and Earth-resources experiments, and on the other hand, the USSR used this civilian programme as a cover for the highly secretive military stations, which flew under the Salyut designation. Salyut 1, the first station in the program, became the world's first crewed space station.

Salyut flights broke several spaceflight records, including several mission-duration records, and achieved the first orbital handover of a space station from one crew to another, and various spacewalk records. The ensuing was vital for evolving space station technology from a basic, engineering development stage, from single docking port stations to complex, multi-ported, long-term orbital outposts with impressive scientific capabilities, whose technological legacy continues . Experience gained from the Salyut stations paved the way for multimodular space stations such as and the International Space Station (ISS), with each of those stations possessing a Salyut-derived core module at its heart.

Mir-2 (DOS-8), the final spacecraft from the Salyut series, became one of the first modules of the ISS. The first module of the ISS, the Russian-made Zarya, relied heavily on technologies developed in the Salyut programme.

(2008). 9780387739731, Springer Science & Business Media. .


History of Salyut space stations
The programme was composed of civilian stations and military stations:

  • The space station cores were designed in October 1964 by Vladimir Chelomey's NPO Mashinostroyeniya (OKB-52) organization as military space stations, long before the Salyut programme started. For Salyut, small modifications had to be made to the docking port of the OPS to accommodate Soyuz spacecraft in addition to TKS spacecraft.
  • The civilian DOS space station cores were designed by 's OKB-1 organisation. Korolev and Chelomey had been in fierce competition in the Soviet space industry during the time of the Soviet crewed lunar programme, but OKB-52's Almaz-OPS hull design was combined with subsystems derived from OKB-1's Soyuz. This was done beginning with conceptual work in August 1969. The DOS differed from the OPS modules in several aspects, including extra solar panels, front and (in Salyut 6 and 7) rear docking ports for Soyuz spacecraft and TKS spacecraft, and finally more docking ports in DOS-7 and DOS-8 to attach further space station modules.

It was realized that the later civilian DOS stations could not only offer a cover story for the military Almaz programme, but could also be finished within one year and at least a year earlier than Almaz. The Salyut programme begun on 15 February 1970 on the condition that the crewed lunar programme would not suffer. However, the engineers at OKB-1 perceived the L3 lunar lander effort as a dead-end and immediately switched to working on DOS. In the end it turned out that the Soviet N1 "Moon Shot" rocket never flew successfully, so OKB-1's decision to abandon the lunar programme and derive a DOS space station from existing Soyuz subsystems and an Almaz/OPS hull proved to be right: The actual time from the DOS station's inception to the launch of the first DOS-based Salyut 1 space station took only 16 months; the world's first space station was launched by the Soviet Union, two years before the American or the first Almaz/OPS station flew.

Initially, the space stations were to be named Zarya, the Russian word for "Dawn". However, as the launch of the first station in the programme was prepared, it was realised that this would conflict with the Zarya of the RKA Mission Control Center (TsUP) in Korolyov – therefore the name of the space stations was changed to Salyut shortly before launch of Salyut 1. Another explanation given is that the name might have offended the Chinese, who purportedly were preparing a new rocket for launch, which they had already named Shuguang or "Dawn".

(2025). 9780160895593, NASA. .
The Salyut programme was managed by ,
(2025). 9780803222922, University of Nebraska Press. .
chairman of the state commission for Soyuz missions.
(2025). 9780387735856, Springer Science+Business Media. .

A total of nine space stations were launched in the Salyut programme, with six successfully hosting crews and setting some records along the way. However, it was the stations Salyut 6 and Salyut 7 that became the workhorses of the programme. Out of the total of 1,697 days of occupancy that all Salyut crews achieved, Salyut 6 and 7 accounted for 1,499. While Skylab already featured a second docking port, these two Salyut stations became the first that actually utilised two docking ports: this made it possible for two Soyuz spacecraft to dock at the same time for crew exchange of the station and for Progress spacecraft to resupply the station, allowing for the first time a continuous ("permanent") occupation of space stations.

The heritage of the Salyut programme continued to live on in the first multi-module space station with the Mir Core Module ("DOS-7"), that accumulated 4,592 days of occupancy, and in the International Space Station (ISS) with the Zvezda module ("DOS-8"), that accumulated 4,310 days of occupancy. Furthermore, the Functional Cargo Block space station modules were derived from the Almaz programme, with the Zarya ISS module being still in operation together with Zvezda.


First generation – The first space stations
The first generation served as a space station engineering test bed. The aim from the beginning of the Almaz program was to construct long-living multi-modular stations.


Salyut 1 (DOS-1)

DOS-2

Salyut 2 (OPS-1, military)

Kosmos 557 (DOS-3)

Salyut 3 (OPS-2, military)
Salyut 3 would make history by conducting the first test-fire of a conventional weapon in space. During Salyut 3’s mission span, cosmonauts would fire the onboard 23mm cannon, which was reported to be a modified Nudelman aircraft cannon. To operate the cannon, the crew had to maneuver the whole space station in the direction of the target. Sources state that the firing was to deplete the ammunition on the craft. However, others sources say that the station conducted 3 tests of the gun through the whole mission span of Salyut 3.Anatoly Zak. "OPS-2 (Salyut-3)". RussianSpaceWeb.com.


Salyut 4 (DOS-4)

Salyut 5 (OPS-3, military)

Second generation – long-duration inhabitation of space
In 1977, another marked step forward was made with the second generation of Salyut stations. The aim was to continuously occupy a space station with long-duration expeditions, for the first time in spaceflight.

Although Salyut 6 and Salyut 7 resembled the previous Salyut stations in overall design, several revolutionary changes were made to the stations and programme for the aim of continuous occupation. The new stations featured a longer design life and a second docking port at the aft of the stations – crew exchanges and station "handovers" were now made possible by docking two crewed Soyuz spacecraft at the same time. Furthermore, the uncrewed Progress resupply craft was created based on the crewed Soyuz, to resupply the crew and station with air, air regenerators, water, food, clothing, bedding, mail, propellants, pressurant, and other supplies. While the Progress docked to the station's second docking port, the crew's Soyuz spacecraft could remain docked to the station's first port. The Progress spacecraft even delivered hardware for updating onboard experiments and permitting repairs to the station, extending its life.


Salyut 6 (DOS-5)

Salyut 7 (DOS-6)

Salyut's heritage – modular space stations
After the second generation, plans for the next generation of Salyut stations called for the cores DOS-7 and DOS-8 to allow, for the first time in spaceflight, the addition of several modules to a station core and to create a modular space station. For this, the DOS modules were to be equipped with a total of four docking ports: one docking port at the aft of the station as in the second generation Salyuts, and the replacement of the front docking port with a "docking sphere" containing three docking ports — front, port, and starboard.

While the station cores DOS-7 and DOS-8 were built and flown, they never received the Salyut designation. Instead, DOS-7 evolved into the Mir Core Module for the Mir space station that followed the Salyut programme, and DOS-8 was used as the Zvezda Service Module for the International Space Station (ISS) which followed Mir.

The heritage from the Almaz programme is present even today. While the last space station from the Almaz programme was flown as Salyut 5 in 1976, the development of the Almaz evolved into the Functional Cargo Block, which formed the basis for several Mir modules, the experimental Polyus orbital weapons platform and the Zarya module of the ISS.


Mir Core Module (DOS-7)
DOS-7 continued to be developed during Salyut 7, becoming the Mir Core Module of the space station – the first modular space station, with crewed operations lasting from 1986 to 2000. The station featured upgraded computers and solar arrays, and accommodations for two cosmonauts each having their own cabin. A total of six docking ports were available on the Mir Core Module, which were used for space station modules and visiting spacecraft – the docking sphere design had been upgraded from its initial Salyut design to contain a maximum of five docking ports (front, port, starboard, zenith and nadir). And finally, the modules for Mir were derived from the Functional Cargo Block design of the Almaz programme.

The name of the Mir space station – , literally Peace or World – was to signify the intentions of the Soviet Union to bring peace to the world. However, it was during the time of Mir that the Soviet Union was dissolved in December 1991, ending what was begun with the 1917 October Revolution in Russia. This dissolution had started with the Soviet " and " ("restructuring and openness") reform campaigns by Soviet leader Mikhail Gorbachev in the 1980s, had reached a preliminary endpoint with the revolutions of 1989 and the end of the communist ( and the ), finally to reach the Soviet Union itself in 1991.

While the Russian Federation became the successor to much of the dissolved and was in a position to continue the Soviet space program with the , it faced severe difficulties: imports and exports had steeply declined as the economic exchange with nations had crumbled away, leaving the industry of the former Soviet Union in shambles. Not only did the political change in eastern Europe signify an end of contributions to the space programme by eastern European nations (such as the Carl Zeiss Jena), but parts of the Soviet space industry were located in the newly independent , which was similarly cash-strapped as and started to demand for its contributions.

It was during this time of transition and upheaval that the Shuttle–Mir program was established between the and the in 1993. The former adversaries would now cooperate, with "Phase One" consisting of joint missions and flights of the United States to the . It was a partnership with stark contrasts – Russia needed an inflow of hard currency to keep their space programme aloft, while in the United States it was seen as a chance to learn from the over 20 years of experience of Soviet space station operations. It was "Phase Two" of this Shuttle–Mir program that would lead to the International Space Station.

(2004). 9781852337100, Springer Science & Business Media. .


Zvezda ISS Service Module (DOS-8)
DOS-8 evolved into the Mir-2 project, intended to replace Mir. Finally, it became the International Space Station (ISS) Zvezda Service Module and formed the core of the early ISS together with the Zarya module (which was derived from Almaz Functional Cargo Block designs).


Data table
The first generation of Salyut stations received few craft for rendezvous and docking. By contrast the programme's second generation stations, Salyut 6 and Salyut 7, received multiple crewed and uncrewed craft for rendezvous, docking attempts (whether successful or not), human habitation, crew transfer, and supply. The table counts craft which achieved rendezvous with their targets as visiting craft, regardless of whether they docked successfully.

Salyut 1DOS-119 April 1971
01:40:00 UTC
11 October 1971
|align="right"
2332
18,500
-DOS-229 July 197229 July 1972|align="right"
18,500
Salyut 2OPS-1 (military)4 April 1973
09:00:00 UTC
28 May 1973
|align="right"
18,500
-
(Kosmos 557)
DOS-311 May 1973
00:20:00 UTC
22 May 1973
|align="right"
19,400
Salyut 3OPS-2 (military)25 June 1974
22:38:00 UTC
24 January 1975
|align="right"
1522
18,500
Salyut 4DOS-426 December 1974
04:15:00 UTC
3 February 1977
|align="right"
9242118,500
Salyut 5OPS-3 (military)22 June 1976
18:04:00 UTC
8 August 1977
|align="right"
6743
19,000
Salyut 6DOS-529 September 1977
06:50:00 UTC
29 July 1982
|align="right"
68333181519,824
Salyut 7DOS-619 April 1982
19:45:00 UTC
7 February 1991
|align="right"
81626111518,900
For comparison, the DOS-7 and DOS-8 modules that were derived from the Salyut programme:
DOS-7
Mir Core Module
19 February 198623 March 2001
|align="right"
4,592104396420,400
ISSDOS-8
Zvezda
ISS Service ModuleAll data for Zvezda (DOS-8) .
12 July 2000
|Still in orbit
8,7237,50021585
65
19,051


See also
  • List of human spaceflights to Salyut space stations
  • List of Salyut expeditions
  • List of Salyut visitors
  • List of Salyut spacewalks
  • List of uncrewed spaceflights to Salyut space stations


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