LK-1 – crewed lunar flyby spacecraft First work on the VA spacecraft began on 13 May 1961 by
Vladimir Chelomey's
OKB-52 design bureau, in response to the
US Apollo program. The VA spacecraft consisted of three main parts: • The VA capsule, which formed the pressurized habitable section for the crew • The NO front compartment (, lit. "nose compartment"), housing the deorbit block (BSO), additional batteries, communication equipment, the parachute and soft landing engines • The SAS
launch escape system () – 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 crewed lunar spacecraft effort, the VA spacecraft was repurposed by Chelomey as support craft for his military Almaz space station program – again a response to a US program, the
USAF's military
Manned Orbiting Laboratory (MOL) and
Gemini B effort.
Almaz APOS 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 been 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 entered the Almaz station 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.
TKS spacecraft For the flights of the subsequent 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 crewed
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 uncrewed 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 still in use for the
Zarya FGB, albeit in modified form. ==Test flights==