TKS (spacecraft)

TKS spacecraft

Soviet TKS crew delivery/cargo ship
Description
Role:	Manned spacecraft to supply the military Almaz space station
Crew:	three
Dimensions
Height:	43.31 ft	13.2 m
Diameter:	13.61 ft	4.15 m
Volume:		45.00 m3
Rocket engines
Main Engine (N2O4/UDMH):	1763 lbf ea	7840 N
Performance
Endurance:	7 days
Apogee:	266 km
Perigee:	223 km
Inclination:	52 degrees
Spacecraft delta v:	2290 ft/s	700 m/s
Cutaway of TKS vehicle
Cutaway of TKS vehicle. Details are conjectural. The broad black line outlines the vehicle’s pressurized compartments. A tunnel (stippled) connects the FGB and VA spacecraft

The TKS spacecraft (Russian: Транспортный корабль снабжения, Transportnyi Korabl’ Snabzheniia, Transport Supply Spacecraft, GRAU index 11F72) was a Soviet spacecraft conceived in the late 1960s for resupply flights to the military Almaz space station.

The spacecraft was designed for both crewed and autonomous uncrewed cargo resupply flights, but was never used operationally in its intended role – only four test missions were flown (including three that docked to Salyut space stations) during the program. The Functional Cargo Block (FGB) of the TKS spacecraft later formed the basis of several space station modules, including the Zarya FGB module on the International Space Station.

The TKS spacecraft consisted of two spacecraft mated together, both of which could operate independently:

• The VA spacecraft (known in the West as the Merkur spacecraft), which would have housed the cosmonauts during launch and reentry of an TKS spacecraft, while traveling to and from an Almaz space station.
• And the Functional Cargo Block (FGB) which, in order to resupply an Almaz space station, carried docking hardware, tanks and a large pressurized cargo compartment. Furthermore, the FGB carried the on-orbit maneuvering engines for the TKS.

While the VA carried the reentry hardware, and only minimal life support and maneuvering systems, the FGB would have been used as the primary orbital maneuvering system and cargo storage for the TKS spacecraft.

The FGB could also be used alone as an unmanned cargo module without an VA spacecraft, which enabled the FGB design to be re-purposed as FGB space station modules later on. The VA spacecraft on the other hand was also intended to be launched as "Almaz APOS", mated with an Almaz-OPS space station core as the primary orbital maneuvering system, instead of a FGB. As of August 2009, Excalibur Almaz planned to use the VA capsule as low-cost cargo return vehicles.

Design

File:TKSmodel1.jpg

A model of an TKS spacecraft. On the left is the cylindrical Functional Cargo Block with attached solar panels. In the middle is the VA spacecraft, with the conical VA return capsule for the crew and the VA's orbital manoeuvring engines in the long nose section. Standing right front is the launch escape system, which would have been attached to the top of the VA's nose section during launch and jettisoned after a successful launch.

The TKS spacecraft was designed by Vladimir Chelomei (the VA capsule) and V. N. Bugayskiy (the FGB block) as a manned spacecraft launched with Proton rocket alternative to the Soyuz spacecraft for use with Almaz space stations. Development began in 1965; the Almaz programme had been abandoned by the time the first TKS spacecraft flew in 1977. The VA spacecraft ("Vozvrashaemiy Apparat") was flown separately on four test missions with two craft per launch to test the design, as well as one "all-up" test mission and three resupply missions.

The project had further evolved with space station "Modulny" ("Modular") based on the TKS design outline, reworked to dock with Salyut 7, Mir and ISS space stations. This development was designated FGB, or Functional Cargo Block.

The TKS spacecraft consisted of an 11F74 "Vozvraschaemyi Apparat" (or Return Vehicle commonly referred to as the VA), attached to an 11F77 "Transportniy Korabl Snabzheniya" (Functional/Cargo Block module or FGB).

TKS VA

Main article: VA spacecraft

The TKS VA spacecraft was itself a very compact and efficient spacecraft. Typically it would reenter the atmosphere within 2 orbits, but could fly autonomously for up to 31 hours. The pressurized crew re-entry capsule was equipped with its own environmental control system, and topped with reaction control system, de-orbit braking engine, parachute system, and soft landing engines. Although extensively flight tested, it never flew with a crew on board.

The VA design was derived from the planned capsule for the Chelomei's LK-1 manned circumlunar spacecraft of the 1960s. It was also the basis for Chelomei's LK-700 Lunar Lander crew capsule. The VA looked somewhat similar to the Apollo capsule, but was 30% smaller than its NASA counterpart.

TKS FGB

Main article: Functional Cargo Block

The FGB was entered from the VA spacecraft via a short tunnel. At the aft end a pilot station was equipped with controls and windows for manual docking with the Almaz space station. The docking port was also located here. Operational TKS spacecraft would have delivered KSI film return capsules to Almaz stations. These would have been stored around the docking port for transfer to the film capsule airlock for loading.

Details

TKS VA return capsule of Kosmos 1443

Specifications

Crew size:	3
Design life:	7 days
Orbital storage:	200 days
Typical orbit:	223 km x 266 km at 52 degrees inclination
Length:	13.2 m (43.31 ft)
Maximum diameter:	4.15 m (13.61 ft)
Span:	17.00 m (55.00 ft)
Habitable volume:	45.00 m3
Mass:	17,510 kg (38,600 lb)
Payload:	12,600 kg (27,700 lb)
Main engine thrust:	7.840 kN (1,763 lbf)
Main engine propellants:	N2O4/UDMH
Main engine propellants:	3,822 kg (8,426 lb)
Main engine Isp:	291 sec
Spacecraft delta v:	700 m/s (2,290 ft/s)
Electrical system:	Solar panels 17 m span 40 m²
Electric system:	2.40 average kW
Associated launch vehicle:	Proton 8K82K

Missions

VA spacecraft test flights

Main article: VA spacecraft § Test flights

Four flights with eight VA spacecraft without an FGB module were conducted to speed up the development of the TKS spacecraft:

• Orbital test of a pair of two VA spacecraft Kosmos 881 and Kosmos 882 in 1976-12-15 that started jointly and reentered on the same day.
• VA #009L/P and VA #009P/P: Launched on 1977-08-04. Launch vehicle failure forty seconds into the flight on a suborbital test of two VA spacecraft. VA #009L/P is destroyed in the resulting booster explosion, VA #009P/P is rescued by the Proton SAS abort system and is recovered safely.
• On 1978-03-30 pair of two VA spacecraft Kosmos 997 and Kosmos 998 started jointly and reentered separately
• On 1979-05-23 pair of two VA spacecraft Kosmos 1100 and Kosmos 1101 that started jointly and reentered separately

TKS-1 (Kosmos 929)

"Kosmos 929" redirects here.

Kosmos 929 was the first flight of a "complete" TKS spacecraft (VA spacecraft with FGB), launched on 17 July 1977 – it was a "solo" test flight and was not destined for a Salyut space station. The VA capsule returned to Earth 16 August 1977. The remainder of the spacecraft – the FGB – deorbited on 2 February 1978.

TKS-2 (Kosmos 1267)

Main article: Kosmos 1267

On 25 April 1981, TKS-2 was launched unmanned as Kosmos 1267, the first FGB to dock with a space station. After separation and recovery of the VA capsule on 24 May 1981, the FGB docked on 19 June with Salyut 6, after 57 days of autonomous flight. It remained attached to the station until both deorbited and were destroyed on 29 July 1982.

TKS-3 (Kosmos 1443)

"Kosmos 1443" redirects here.

On 2 March 1983, TKS-3 was launched unmanned as Kosmos 1443. This time, the VA remained attached and the first "complete" TKS docked to Salyut 7 two days after launch. TKS-3 separated from the station on 14 August. After undocking, the FGB and the VA spacecraft separated and the VA spacecraft continued in space for four more days demonstrating autonomous flight, before the VA capsule successfully re-entered on 23 August 1983, landing 100 km south-east of Arkalsk and returning 350 kg of material from the station. The FGB deorbited itself on 19 September 1983.

TKS-4 (Kosmos 1686)

Main article: Kosmos 1686

A drawing of the last flown TKS spacecraft, Kosmos 1686, depicted docked to the Salyut 7 space station. The VA capsule is visible on the bottom left. The "nose section" of the VA spacecraft, that would have contained the de-orbit engines for the VA capsule, has been replaced with remote sensing instruments.

TKS-4 was launched unmanned as Kosmos 1686 on 27 September 1985. The landing systems, ECS, seats, and manned controls were removed from the VA spacecraft, and instead other payload was installed: a high-resolution photo apparatus, an infrared telescope and the Ozon spectrometer). The TKS successfully docked with Salyut 7.

The "military" long duration crew Salyut 7 EO-4, consisting of Viktor Savinykh, Alexander Volkov and the commander Vladimir Vasyutin, had manned Salyut 7 that month to conduct experiments with TKS-4. Commander Vasyutin fell ill soon after arriving at the station. Originally scheduled to have a six-month stay aboard Salyut 7, Vasyutin's illness forced the crew to make an emergency return to Earth on 21 November 1985, preventing the crew from finishing the TKS experiments. The crew of Soyuz T-15 returned to Salyut 7 in May 1986, to conclude some of the experiments and ferry equipment to the then new Mir space station.

Salyut 7 was moved to a higher orbit after that mission, while awaiting another 'TKS' crew – there were even plans to return using the Buran shuttle. Such flights never materialized before Salyut 7 and Kosmos 1686 deorbited on 7 February 1991, burning up together over Argentina.

Further usage

Main article: Functional Cargo Block

The TKS design, which has never been flown manned, has gone on to provide the basic structure for several later space station components, such as:

• Kvant-1 tug
• Kvant-2 Mir module
• Kristall Mir module
• Spektr Mir module
• Priroda Mir module
• Polyus (FGB) spacecraft
• Zarya (FGB-1) ISS module
• Russian Research Module (FGB-2) ISS module (canceled)
• Multipurpose Laboratory Module (FGB-2) ISS module

Two TKS/Almaz VA capsules were bought for commercial use, by the private spaceflight company, Excalibur Almaz. As of 2014 one of those were auctioned for 1 million euro, and the other was reportedly shipped away from the company's headquarters on Isle of Man in an undisclosed direction.

Gallery

TKS based and descendant spacecraft and modules.

• TKS spacecraft drawing.png

  Soviet TKS crew delivery/cargo ship

• TKS cutaway.png

  Cutaway of TKS vehicle. Details are conjectural

• 

  Kosmos 1686. Note the VA capsule (left), heavily modified to house scientific instruments

• Salyut 7 and Cosmos 1686 drawing.png

  Kosmos 1686 and Salyut 7

• 

  Polyus cutaway

• 

  Kvant-1 with its orbital tug attached

• 

  Cut-way view of Kvant-2

• 

  Cut-way view of Kristall

• Spektr - Mir module.png

  Cut-away view of Spektr

• 

  Cut-away view of Priroda

• 

  Zarya module as seen from STS-88

• 

  MLM docked to the ISS

See also

• Big Gemini - Planned U.S. equivalent to the TKS spacecraft
• Manned Orbiting Laboratory - U.S. Air Force equivalent to Almaz space station
• TKS-based spacecraft

Further reading

• RussianSpaceWeb.com: OPS-4 space station

External links

• http://www.astronautix.com/craft/tks.htm
• http://www.russianspaceweb.com/tks.html