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 maneuvering 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 was designed under
Vladimir Chelomey (VA capsule) and V. N. Bugayskiy (FGB block) as a crewed alternative to the
Soyuz spacecraft for servicing
Almaz stations, launched on the
Proton rocket. Development began in 1965, but by the time the first TKS flew in 1977 the
Almaz programme was already winding down. Four test flights of the VA capsule were conducted without the FGB to validate the design, each launching two capsules stacked together. On one flight the launch vehicle exploded, destroying the lower capsule, while the upper capsule successfully used its
launch escape system. Four flights of the complete TKS (VA with FGB) were also launched: one as a systems test, and three that docked with
Salyut stations to deliver cargo. The FGB could also be launched independently as an autonomous uncrewed cargo module, a role that led to its adaptation as the basis for later space station modules. The VA was likewise considered for the "Almaz APOS" concept, in which a crew would have launched docked to an Almaz core inside a VA capsule.
TKS VA The VA was a compact reentry capsule derived from Chelomei's earlier
LK-1 circumlunar spacecraft and
LK-700 lunar lander capsule designs. It resembled the
Apollo Command Module but was about 30% smaller. The pressurized capsule carried its own
life-support system,
reaction control thrusters, deorbit engine,
parachutes, and soft-landing rockets. It could operate autonomously for up to 31 hours and typically reentered within two orbits. In addition to a three-person crew, the VA could return up to of cargo, mainly KSI film-return capsules. Unusually, its docking hatch was located on the aft side, requiring crews to enter and exit through an opening in the
heat shield. Although extensively flight-tested, no VA ever carried a crew.
TKS FGB The FGB provided cargo space, docking hardware, and the main orbital maneuvering engines. Crews accessed it through a short tunnel from the VA. At its aft end was a pilot station with controls and windows for manual docking with an Almaz station. Planned operational TKS flights would also have delivered KSI film-return capsules, stowed near the docking port and transferred to the VA spacecraft for return to Earth. == Details ==