TKS spacecraft
Welcome to our website. It is generaly simplier version of wikipedia. You will find there selected articles. Enjoy!
| 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 capsule |
||
| TKS spacecraft | ||
TKS spacecraft was designed by Vladimir Chelomei as a manned spacecraft launched with Proton rocket alternative to the Soyuz spacecraft to supply the military Almaz space station. Development began in 1965, but by the time the first flight articles were ready the Almaz programme had been abandoned. The VA ("Vozvrashaemiy Apparat") capsule was flown separately on four test missions with two capsules on one booster to test the design, as well as one "all-up" test mission and three resupply missions. It was never flown manned, although in December 1978 formation of a special group of six cosmonauts was approved for manned missions on board the TKS spacecraft.
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.
Excalibur Almaz plans to use the Reusable Return Capsule portion of the TKS spacecraft for commercial purposes. These capsules will be fitted with small service modules - each designed according to its mission parameters.
Contents |
Design
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
The TKS VA 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 (similar to the American Apollo but 30% smaller) 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 (due to political rivalry).
The VA was derived from an earlier capsule designed for the Chelomei's planned LK-1 manned circumlunar spacecraft of the 1960s. It was also the basis for Chelomei's LK-700 Lunar Lander crew capsule.
TKS FGB
The FGB was entered from the VA capsule 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 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
| 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
Cosmos 881 and Cosmos 882
Orbital test of a pair of two VA capsules in 1976-12-15 that started jointly and reentered separately.
TKS-1 (Cosmos 929)
Lone flight of full TKS-1 with FGB and VA capsule. Launched 1977-07-17. The VA capsule returned to Earth 1977-08-16. The remainder of the spacecraft deorbited 1978-02-02.
Unnamed
Launched at 1977-08-05. Launch vehicle failure on a suborbital test of two VA capsule.
Cosmos 997 and Cosmos 998
On 1978-03-30 pair of two VA capsules that started jointly and reentered separately
Cosmos 1100 and Cosmos 1101
On 1979-05-23 pair of two VA capsules that started jointly and reentered separately
TKS-2
On April 25, 1981, TKS-2 was launched unmanned as Cosmos 1267. The VA capsule was recovered on 24 May 1981. The FGB docked with Salyut 6 on June 19 after 57 days of autonomous flight. It remained attached to the station until both deorbited and were destroyed on 29 July 1982.
TKS-3
On 2 March 1983, TKS-3 was launched unmanned as Cosmos 1443. This time, the VA remained attached and the TKS docked to Salyut 7 two days after launch. TKS-3 separated from the station on 14 August. The VA re-entry capsule separated and deorbited itself on 19 September 1983. The VA capsule continued in space for four more days demonstrating autonomous flight, before successfully re-entering on 23 August 1983, landing 100 km south-east of Arkalsk and returning 350 kg of material from the station.
TKS-4
TKS-4 was launched unmanned as Cosmos 1686 on 27 September 1985. In the VA capsule landing systems, the ECS, seats, and manned controls were removed and replaced with a high-resolution photo apparatus and optical sensor experiments (infrared telescope and Ozon spectrometer). The TKS successfully docked with Salyut 7. After 21 November 1985, Salyut 7 was moved to a higher orbit while awaiting the second 'TKS' crew, but control of the station was lost. There were plans to return using the Buran shuttle for inspection, but the first flight of the spaceplane was delayed. Salyut 7 and Cosmos 1686 burned up in the atmosphere together in a fiery show over Argentina on 7 February 1991.
Further usage
The TKS design, which has never been flown manned, has gone on to provide the basic structure for several space future 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
- Multipurpose Laboratory Module (FGB-2) ISS module
TKS/Almaz VA capsules are presently being modernized for commercial use, by the private spaceflight company, Excalibur Almaz.
Gallery
TKS based and descendant spacecraft and modules.
|
Soviet TKS crew delivery/cargo ship |
Cutaway of TKS vehicle. Details are conjectural |
 Cosmos 1686. Note the Merkur capsule (left), heavily modified to house scientific instruments |
 Cosmos 1686 and Salyut 7 |
 Polyus cutaway |
 Kvant-1 with its orbital tug attached |
 Cut-way view of Kvant-2 |
 Cut-way view of Kristall |
 Cut-away view of Spektr |
 Cut-away view of Priroda |
 Zarya module as seen from STS-88 |
 MLM docked to the ISS |
See also
- Merkur capsule
- Almaz
- Zarya
- 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
- Kvant
- Kvant-2
- Kristall
- Spektr
- Priroda
- Polyus
References
External links
 |
Wikimedia Commons has media related to: TKS spacecraft |
- http://www.astronautix.com/craft/tks.htm
- http://www.russianspaceweb.com/tks.html
Sources
- http://www.russianspaceweb.com/almaz_ops4.html
|
|||||||||||||
|
|||||||||||||
|
||||||||||||||||||||||
|
||||||||||||||||
Thanks for your time.