Cosmos 1686 (TKS)

Launch Success

Liftoff Time (GMT)

08:41:42

Friday September 27, 1985

Mission Details

Launch Notes

Last flight of the TKS capsule.

Cosmos 1686

Wiki

The TKS spacecraft (Russian: Транспортный корабль снабжения) 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 mistakenly in the West as the Merkur spacecraft), which would have housed the cosmonauts during launch and reentry of a 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 uncrewed cargo module without a 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 an FGB. This specific ship was an uncrewed TKS spacecraft which replaced landing and environmental control systems and seats with some scientific instruments including an infrared telescope and the Ozon spectrometer. Docked with Salyut-7.

Low Earth Orbit

1 Payload

17,510 kilograms

Rocket

Retired
Proton-K

Active 1968 to 2000

Khrunichev State Research and Production Space Center logo

Manufacturer

Khrunichev

Rocket

Height: 56.14m

Payload to Orbit

LEO: 20,100 kg

GTO: 0 kg

Liftoff Thrust

9,469 Kilonewtons

Fairing

Diameter: 4.15m

Height: 16.12m

Stages

3

Launch Site

Site 200/39

Baikonur Cosmodrome, Kazakhstan

Fastest Turnaround

10 days 23 hours

Stats

Proton-K


129th

Mission

7th

Mission of 1985

Khrunichev State Research and Production Space Center


1941st

Mission

72nd

Mission of 1985

1985


89th

Orbital launch attempt