The Vozvraschaemyi Apparat (Russian: Возвращаемый Аппарат ВА, Return Vehicle, GRAU index 11F74), or VA spacecraft, was a Soviet crew capsule, intended to serve as a manned launch and reentry vehicle. Initially designed for the LK-1 manned lunar flyby spacecraft for one of the Soviet manned lunar programs, then the LK-700 redesign, it was later repurposed for the Almaz military space station program. The VA capsule on display at the Smithsonian National Air and Space Museum was labeled as Merkur, following a mistranslation of the original documentation – while incorrect, the name is being used in the West for the VA spacecraft and capsule.
The VA spacecraft was capable of independent flight – up to 31 hours in its last incarnation – it needed however to be combined with additional hardware (containing propulsion and storage) to achieve a longer flight duration. Three different such usage scenarios for the VA spacecraft were planned: Initially the LK-1 spacecraft, and after LK-1's cancellation the plans for Almaz APOS and the TKS spacecraft utilized the VA spacecraft.
- For the lunar flyby spacecraft LK-1, the plans by Vladimir Chelomey's design bureau OKB-52 were to mate an VA spacecraft together with an Equipment-Rocket System Block (PAB) and the Translunar Injection Stage (RB).
For the Almaz program, the plans envisaged two configurations for the crewed VA spacecraft:
- A VA spacecraft would have launched the initial crew of an Almaz-OPS space station, the VA spacecraft launched together with the station itself; This combination was known as "Almaz APOS".
- A VA spacecraft would have been launched mated together with an Functional Cargo Block (FGB) to resupply an Almaz station, in both crewed and uncrewed flights; This combination was known as the TKS spacecraft.
While the VA spacecraft has seen some successful uncrewed test flights, both with and without an Functional Cargo Block, it never served in its intended role as a lunar or Almaz crew vehicle when the programs was canceled, and neither was it ever launched together with an Almaz space station.
- 1 Design
- 2 Test flights
- 3 Specifications
- 4 Excalibur Almaz
- 5 See also
- 6 External links
- 7 References
LK-1 – manned lunar flyby spacecraft
- The VA capsule, which formed the pressurized habitable section for the crew
- The NO front compartment (Russian: Носовой Отсек НО, lit. "nose compartment"), housing the deorbit block (BSO), additional batteries, communication equipment, the parachute and soft landing engines
- The SAS launch escape system (Russian: Система Аварийного Спасения САС) – similar to Soyuz and Apollo – mounted on top of the nose section, jettisoned after first stage had burned out
Cosmonaut Alexei Leonov called the Almaz VA return capsule "our Apollo". The shape of the VA capsule was vaguely like that of the Apollo Command Module (CM), however some of the VA's support hardware was housed on top of the capsule in the nose compartment – unlike Apollo with the Apollo Service Module (SM) below the Apollo CM.
While the VA spacecraft was capable of independent flight of about one day, it needed to be mated to additional hardware for a longer flight duration. For a lunar mission, the LK-1 spacecraft would have been formed by mating the VA spacecraft with two components:
- The Equipment-Rocket System Block (PAB). It included – analogous to the Apollo's SM – solar panels and electrical power systems, communications systems like a parabolic antenna and thrusters for midcourse maneuvers.
- The Translunar Injection Stage (RB).
Almaz space station support craft
After the cancellation of the LK-1 manned lunar spacecraft effort, the VA spacecraft got repurposed by Chelomey as support craft for his military Almaz space station program – again a response to an US program, the USAF's military Manned Orbiting Laboratory (MOL) and Gemini B effort.
The initial plans called for crew and station to be launched together with one Proton rocket launch, just like the US MOL/Gemini combination. For this a VA spacecraft would have being mated on top of an Almaz OPS space station core (11F71) – this was known as Almaz APOS. The crew would have ridden into space in the VA capsule; Once in orbit, the crew would have manned the Almaz station by entering it through a hatch in the heat shield – just like MOL/Gemini. The VA capsule would then remain unoccupied until the end of the mission, when it would serve as the reentry vehicle for the crew. The Almaz APOS concept evolved into the Almaz-OPS stations of the Salyut programme, which were however never launched together with their crew, nor together with a VA capsule.
For the flights of the subsequential crews of an Almaz space station, the VA spacecraft would have been mated with a Functional Cargo Block (FGB, 11F77) instead. Together the VA and the FGB would form the manned TKS spacecraft (11F72) for crew and resupply flights to Almaz space stations – the VA would serve in its role as launch and reentry vehicle for the crew, while the FGB would serve as a propulsion system, pressurized cargo carrier and contain the docking hardware.
A few TKS spacecraft flew unmanned missions, but never to an Almaz-OPS station. The FGB would however continue to find use and form the basis for several space station modules – the FGB concept is as of 2012[update] still in use for the Zarya FGB, albeit in modified form.
Although the VA was never launched crewed, never together with an Almaz-OPS station, and never to an Almaz-OPS station, it saw several flights, some in the intended TKS spacecraft configuration: To accelerate the man-rating of the TKS and VA spacecraft, eight unmanned VA spacecraft (without FGBs) were launched in pairs, testing two VA spacecraft per test flight. One of these flights was aborted due to the carrier rocket failure, and the VA capsule was successfully carried away from the exploding rocket by the launch escape system.
Another four unmanned VA spacecraft were mated together with an FGB and launched as TKS spacecraft: the solo flight of Kosmos 929, the Kosmos 1267 flight to Salyut 6 and the flights of Kosmos 1443 and Kosmos 1686 to Salyut 7 – the VA spacecraft on the TKS flight of Kosmos 1686 was modified as a no-reentry laboratory segment.
VA spacecraft test flights
Kosmos 881 and Kosmos 882
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.
Kosmos 997 and Kosmos 998
Kosmos 1100 and Kosmos 1101
TKS-1 (Kosmos 929)
Kosmos 929 was the first flight of a "complete" TKS spacecraft (VA spacecraft with FGB) on July 17, 1977.
TKS-2 (Kosmos 1267)
TKS-3 (Kosmos 1443)
TKS-4 (Kosmos 1686)
- Mass at launch (including SAS launch escape system): 7,200 to 7,300 kilograms (15,900 to 16,100 lb)
- Mass in orbit: 4,800 kilograms (10,600 lb)
- Gross mass: 3,800 kilograms (8,400 lb)
- Launch payload: 1,880 kilograms (4,140 lb)[dubious ]
- Return payload: 3 persons and 50 kilograms (110 lb), or 500 kilograms (1,100 lb) uncrewed
- Height at launch (including SAS): 10.3 metres (34 ft)
- Height in orbit: 7.3 metres (24 ft)
- Diameter: 2.79 metres (9 ft 2 in)
- Independent operation: up to 31 hours
- First flight: December 15, 1976, as VA spacecraft ("twin" solo flights Kosmos 881 and Kosmos 882)
- Last flight: September 27, 1985, as TKS spacecraft (Kosmos 1686)
- Crew size: 1 for LK-1, 3 for TKS
- Total internal volume: 8.37 cubic metres (296 cu ft)
- Habitable volume: 4.56 cubic metres (161 cu ft)
- Diameter: 2.79 metres (9 ft 2 in)
- Reusable for 10 flights
An TKS spacecraft consisted of a VA spacecraft mated to an Functional Cargo Block (FGB). The specifications of the TKS spacecraft were as follows:
- Mass at launch: 21,620 kilograms (47,660 lb)
- Mass in orbit: 17,570 kilograms (38,740 lb)
- Payload (total): 12,600 kilograms (27,800 lb) (including consumables and VA spacecraft)
- Payload (dry cargo): about 5,200 kilograms (11,500 lb)
- Payload (fuel): 3,822 kilograms (8,426 lb)
- Height: 17.51 metres (57.4 ft)
- Span: 17.00 metres (55.77 ft)
- Thrust: 7.84 kilonewtons (1,760 lbf)
- Electric power: 2.40 kilowatts (3.22 hp) on average
The company Excalibur Almaz acquired four VA return capsule hulls and two Almaz space station hulls. The company plans to outfit and launch both the VA capsules and the Almaz station hulls; One VA capsule is planned to be used in support of space tourism while the other three VA capsules are reserved for scientific and commercial payloads. The needed development of propulsion systems for the VA capsule was reportedly delegated to an unnamed European organization as early as 2009.
- Encyclopedia Astronautica:
- Sven Grahn: The Almaz Space Station Program
- Smithsonian – National Air and Space Museum: Merkur Capsule – Image Detail, showing an VA capsule and its interior
- Novosti Kosmonavtiki: Другой корабль (Online at archive.org, in Russian) The other spacecraft; The 25th anniversary of the first TKS flight.
- "TKS transport ship 11F72". RussianSpaceWeb.com. Retrieved 30 August 2012.
- "TKS-VA (11F74)". Gunter's Space Page. Retrieved 1 September 2012.
- "TKS". Encyclopedia Astronautica. Retrieved 31 August 2012.
- "Space Race". Smithsonian – National Air and Space Museum. Retrieved 1 September 2012.
- "Merkur Capsule – Image Detail". Smithsonian – National Air and Space Museum. Retrieved 1 September 2012.
- "NASM: Nobody's Perfect.". Almaz OPS-5 blog. Retrieved 1 September 2012.
- "LK-1". Encyclopedia Astronautica. Retrieved 2 September 2012.
- "Almaz APOS". Encyclopedia Astronautica. Retrieved 31 August 2012.
- Другой корабль (in Russian). Novosti Kosmonavtiki. Archived from the original on 7 June 2009. Retrieved 2 September 2012.
- "TKS BSO". Encyclopedia Astronautica. Retrieved 2 September 2012.
- "TKS VA". Encyclopedia Astronautica. Retrieved 2 September 2012.
- "TKS SAS". Encyclopedia Astronautica. Retrieved 2 September 2012.
- "Almaz Excalibur". RussianSpaceWeb.com. Retrieved 30 August 2012.