Salyut 1 was adapted from anAlmaz airframe and comprised five components: a transfer compartment, a main compartment, two auxiliary compartments, and theOrion 1 Space Observatory. It was visited by theSoyuz 10 andSoyuz 11 missions. While the crew of Soyuz 10 was able to soft dock, thehard-docking failed, forcing the crew to abort their mission. The Soyuz 11 crew successfully docked, spending 23 days aboard Salyut 1 conducting experiments. The Soyuz 11 crew died of asphyxia caused by a valve failure just before reentry, making them the only humans to have died above theKármán line.
Following the deaths, the mission of Salyut 1 was terminated, and the station reentered Earth's atmosphere, burning up on October 11, 1971.
Salyut 1 originated as a modification of the Soviet military'sAlmaz space station program that was then in development.[2] After the landing ofApollo 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 theN-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 USSkylab 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 throughMir.[2]
Civilian Soviet space stations were internally referred to as DOS (Durable 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 Svinetsradiometer.[6][self-published source]
Construction of Salyut 1 began in early 1970, and after nearly a year it was shipped to theBaikonur Cosmodrome. Some remaining assembly had yet to be done, and this was completed at the launch center. The Salyut programme was managed byKerim Kerimov,[7] chairman of the state commission for Soyuz missions.[8]
Launch was planned for April 12, 1971 to coincide with the 10th anniversary ofYuri Gagarin's flight onVostok 1, but technical problems delayed it until April 19.[9] The first crew launched later in theSoyuz 10 mission, but they ran into troubles while docking and were unable to enter the station; the Soyuz 10 mission was aborted and the crew returned safely to Earth. A replacement crew launched onSoyuz 11 and remained on board for 23 days. This was the first time in the history of spaceflight that a space station had been occupied, and a new record was set for time spent in space. This success was, however, short-lived when the crew was killed duringreentry, as a pressure-equalization valve in the Soyuz 11 reentry capsule had opened prematurely, causing the crew to asphyxiate. They were the first and, as of 2025, only humans to have died in space. After this accident, all missions were suspended while the Soyuz spacecraft was redesigned. The station was intentionally destroyed byde-orbiting after six months in orbit, because it ran out of fuel before a redesigned Soyuz spacecraft could be launched to it.[10]
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]
The transfer compartment was equipped with the onlydocking port of Salyut 1, which allowed oneSoyuz 7K-OKS spacecraft to dock. It was the first use of the SovietSSVP 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]
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] The interior design used various colors (light and dark gray, apple green, light yellow) for supporting the cosmonauts’ orientation in weightlessness.[11]
The third pressurized compartment contained the control and communications equipment, the power supply, thelife 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 ofsolar cell panels that extended like wings from the smaller compartments at each end, the heat regulation system'sradiators, and orientation and control devices.[1]
Salyut 1 was modified from one of theAlmaz airframes. The unpressurized service module was the modified service module of a Soyuz craft.[2]
The only spacecraft that ever docked to Salyut 1 wereSoyuz 10 andSoyuz 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.
Still frame from an animation of Salyut 1 with attached Soyuz.
Soyuz 10 was launched on April 22, 1971, carrying cosmonautsVladimir Shatalov,Aleksei Yeliseyev, andNikolai 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]
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 inKazakhstan, 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 wearingpressure 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]
Salyut 1 was moved to a higher orbit in July–August 1971 to ensure that it would not be destroyed prematurely throughorbital 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 thePacific 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 theelectromagnetic spectrum.[1]
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated inunderline. Uncatalogued launch failures are listed initalics. Payloads deployed from other spacecraft are denoted in (brackets).