Salyut 6

Infobox Space station
station = Salyut 6
station_

station_image_size =
station_image_caption = Salyut 6 with docked Soyuz and Progress spacecraft
insignia = Salyut-6.gif
insignia_caption = Salyut 6 insignia.
sign = Salyut 6
crew = 3
launch = 1977-09-29
06:50:00 UTC
launch_pad = Baikonur Cosmodrome, USSR
reentry = 1982-07-29
mass = 19,824 kilograms
length = 15.8 metres
diameter = 4.15 metres
volume = 90 metres³
perigee = 219 kilometres (136 miles)
apogee = 275 kilometres (171 miles)
inclination = 51.6 degrees
period = 89.1 minutes
orbits_day = 16.16
in_orbit = 1,764 days
occupied = 683 days
orbits = 28,024
distance = ~1,136,861,930 km
(~706,413,253 mi)
as_of = deorbit on 1982-07-29
stats_ref = cite book
last = Harland
first = David
authorlink = David Harland
title = The Story of Space Station Mir
publisher = Springer-Praxis
date = 2005-02-14
location = Glasgow, United Kingdom
url =http://www.amazon.co.uk/Story-Space-Station-Mir/dp/0387230114/ref=sr_1_1/202-3649698-1866219?ie=UTF8&s=books&qid=1183037125&sr=8-1
id = 978-0387230115] [cite web |url=http://nssdc.gsfc.nasa.gov/nmc/masterCatalog.do?sc=1977-097A |title=NASA - NSSDC - Spacecraft - Details |accessdate=2008-06-29 |publisher=NASA |date=2008-04-02 ]
configuration_

---

configuration_size = 190px
configuration_caption = Basic orbital configuration of Salyut 6

Salyut 6 ( _ru. Салют-6; lit. "Salute 6") was a Soviet orbital space station, the eighth flown as part of the Salyut programme. Launched on September 29, 1977 by a Proton rocket, the station was the first of the 'second-generation' type of space station. Salyut 6 possessed several revolutionary advances over the earlier Soviet space stations, which she [Pronouns "she" and "her" are used in this article for the "space station". This choice is motivated by the frequent use of these pronouns by both English and Russian speaking people. [http://ask.yahoo.com/20060627.html Why are boats and ships always referred to as "she"? Ask Yahoo!] ] nevertheless resembled in overall design. These included the addition of a second docking port, a new main propulsion system and the station's primary scientific instrument, the BST-1M multispectral telescope. The addition of the second docking port made crew handovers and station resupply by unmanned Progress freighters possible for the first time, which in turn allowed the programme to evolve from short-duration station visits to long-duration expeditions, marking the beginning of the transition to multi-modular, long-term research stations in space.

From 1977 until 1982 Salyut 6 was visited by five long- and eleven short-duration crews, including cosmonauts from Warsaw Pact countries as part of the Intercosmos programme. The very first long-duration crew to visit the station broke a long-standing endurance record set on board the American Skylab station, staying 96 days in orbit, whilst the longest expedition lasted 185 days. These crews were responsible for carrying out the primary missions of Salyut 6, including astronomy, Earth-resources observations and the study of human adaptation to space. Following the completion of these missions and the launch of her successor, Salyut 6 was deorbited on July 29, 1982, almost five years after her launch. [cite book
last = Baker
first = Philip
authorlink = Philip Baker
title = The Story of Manned Space Stations: An Introduction
publisher = Springer-Praxis
date = 2007-06-01
location = New York, United States of America
url = http://www.amazon.co.uk/Story-Manned-Space-Stations-Introduction/dp/0387307753/ref=sr_1_2?ie=UTF8&s=books&qid=1217856985&sr=8-2
id = 978-0387307756]

Description

Salyut 6, launched on a Proton 8K82K rocket on 1977-09-29,cite web
title = Salyut 6
publisher = Encyclopedia Astronautica
author-link = Mark Wade
first = Mark
last = Wade
url = http://www.astronautix.com/craft/salyut6.htm
accessdate = 2007-07-05 ] marked the switch from engineering development stations to routine operations, and united the most effective elements from each of the previous stations. Her navigation system, made up of 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 4, as was her power system, which consisted of a trio of steerable solar panels together producing a peak of 4 kilowatts of power over 51 metres². The station's thermal regulation systems, which made use of a sophisticated arrangement of insulation and radiators, was also derived from that used on Salyut 4. In addition, Salyut 6 made use of environmental systems first used on Salyut 3, and controlled her orientation using gyrodenes first tested on that station.

.

The rearward of the two ports was fitted with plumbing to allow the station to be refuelled by unmanned Progress spacecraft. These freighters, which 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.

The addition of the extra docking port caused the adoption of the Almaz-derived twin-chamber propulsion system first used on Salyut 3 and 5, with the two engine nozzles—each producing 2.9 kilonewtons of thrust—mounted peripherally on either side of the aft port. Salyut 6 introduced a Unified Propulsion System, with both the engines and the station's control thrusters running on unsymmetrical dimethylhydrazine and nitrogen tetroxide, drawn from a common set of pressurised tanks, allowing the refuelling capabilities of the visiting Progress tankers to be exploited to the maximum effect. The entire engine and fuel storage assembly was contained within an unpressurised bay at the rear of the station, which was the same diameter as the main pressurised compartment. However, the replacement of the Soyuz engine used on previous stations with the bay meant that the station kept a similar overall length to its predecessors.

To enable spacewalks, Salyut 6 was equipped with an inward-opening EVA hatch for on the side of the forward transfer compartment, which could be used as an airlock in a similar way to the system used on Salyut 4. This compartment contained two new semi-rigid spacesuits which allowed much greater flexibility than earlier suits, and could be donned within five minutes in case of an emergency. Finally, the station offered considerable improvements in living conditions over previous outposts, with machinery being soundproofed, the crews being provided with designated 'cots' for sleeping and the equipping of the station with a shower and extensive gymnasium.

Instruments

The primary instrument carried aboard the station was the BST-1M multispectral telescope, which could carry out astronomical observations in the infrared, ultraviolet and submillimetre spectra using a 1.5 metre-diameter mirror which was operated in cryogenic conditions at around −269°C. The telescope could be operated only when Salyut 6 was on the night side of the Earth, and had its cover closed for the rest of the time.

The second major instrument was the MKF-6M multispectral camera, which carried out Earth-resources observations. An improved form of a camera first tested on Soyuz 22, the camera captured an area of 165×220 kilometres with each image, down to a resolution of 20 metres. Each image was captured simultaneously in six bands in 1200-frame cassettes, which required regular replacement due to the fogging effects of radiation. Salyut 6 also featured a KATE-140 stereoscopic topographic mapping camera with a focal length of 140 milimetres, which captured images of 450×450 kilometres with a resolution of 50 metres in the visible and infrared spectra, which could be operated either remotely or by the resident crews. The photographic capabilities of the station were, therefore, extensive, and the Soviet Ministry of Agriculture had planted a number of specifically-selected crops at test sites at Salsky in the Ukraine and Voronezh near Lake Baikal to examine the capabilities of the cameras.

To further expand its scientific capabilities, Salyut 6 was 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 her flight, a Progress spacecraft delivered an external telescope, the KRT-10 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.

upport craft

Salyut 6 was primarily supported by the manned Soyuz spacecraft, which carried out crew rotations and would also have been used in the event of an emergency evacuation. The ferries docked automatically to the station, making use of the new Igla automatic docking system, and were used by departing crews to return to Earth at the end of their flight.cite book
last = Hall & Shayler
title = Soyuz: A Universal Spacecraft
publisher = Springer-Praxis
date = 2003-05-07
location = London, United Kingdom
url =http://www.amazon.co.uk/Soyuz-Universal-Spacecraft-Springer-Praxis-Books/dp/1852336579/ref=sr_1_2?ie=UTF8&s=books&qid=1217856244&sr=8-2
id = 978-1852336578]

The station was the first to be able to be resupplied by the newly-developed unmanned Progress freighters, although they could only dock at the rear port, as the plumbing which allowed the spacecraft to replenish the station's fluids was not available at the front port. The freighters docked automatically to the station via the Igla, and were then opened and emptied by the cosmonauts on board, whilst transfer of fuel to the station took place automatically under supervision from the ground.

In addition to the Soyuz and Progress spacecraft, after her final crew had left, Salyut 6 was visited by an experimental transport logistics spacecraft called Cosmos 1267 in 1982. The transport logistics spacecraft, known as the TKS, was originally designed for the Almaz programme, and proved that large modules could dock automatically with space stations, a major step toward the construction of multimodular stations such as "Mir" and the International Space Station. [cite paper
author = David S. F. Portree
title = Mir Hardware Heritage
publisher = NASA
date = March 1995
url = http://ston.jsc.nasa.gov/collections/TRS/_techrep/RP1357.pdf
format = PDF
accessdate = 2007-03-30] [cite web
title = Cosmos 1267
publisher = Encyclopedia Astronautica
date =
last = Wade
first = Mark
authorlink = Mark Wade
url = http://www.astronautix.com/details/cos72689.htm
accessdate = 2007-06-28]

tation operations

Docking operations

"Dates and times are 24-hour Coordinated Universal Time. Source: "

References