Kosmos 1686

Currently, Kosmos 1686 is a topic that has acquired significant relevance in society. Its impact has been noted in different aspects of daily life, generating discussions and debates in various areas. Whether on a personal, academic or professional level, Kosmos 1686 has managed to capture the attention of a wide spectrum of people, arousing both interest and uncertainty. In this article, we will thoroughly explore the different aspects of Kosmos 1686, analyzing its origin, evolution and consequences, in order to provide a broad and critical vision of this topic that is so relevant today.

Kosmos 1686
Kosmos 1686 (top) docked to Salyut 7, imaged by Range-Doppler radar.
Salyut program insignia
Station statistics
COSPAR ID1985-086A
SATCAT no.16095Edit this on Wikidata
Call signSalyut 7
Launch1985-09-27
02:01:00 UTC
Docked to Salyut 7 on 1985-10-02.
Launch padBaikonur 200/39
ReentryFebruary 7, 1991
Mass20,000 kg
Length15 m
Width16 m
Diameter4.15 m
Periapsis altitude219 km (118.25 nmi)
Apoapsis altitude278 km (150.1 nmi)
Orbital inclination51.6 degrees
Orbital period89.2 minutes
Orbits per day16.14
Days in orbit1959 days
Statistics as of deorbit & reentry
References:[1][2]
Configuration
Combined Kosmos 1686-Salyut 7 space station complex

Kosmos 1686 (Russian: Космос 1686 meaning Cosmos 1686), also known as TKS-4, was a heavily modified TKS spacecraft which docked unmanned to the Soviet space station Salyut 7 as part of tests to attach scientific expansion modules to stations in Earth orbit. The module which docked to the station was the FGB component of a TKS vehicle launched on September 27, 1985, and was designed to test systems planned for use on the Mir Core Module. The spacecraft docked with Salyut 7 on October 2, 1985, during the long-duration stay of the cosmonauts of its fifth principal expedition, which arrived on Soyuz T-14.[2] It was the last flown TKS spacecraft.

Notable features

  • The spacecraft's VA capsule was greatly modified to carry instruments – the retrorocket and parachute packages were replaced by scientific equipment, including an infrared telescope and the Ozon spectrometer.[2]
  • The combined Salyut 7-Kosmos 1686 complex massed 43 tons, with Kosmos 1686 delivering 4500 kg of cargo to Salyut 7 and nearly doubling the amount of habitable volume available to the station's crew.[2]
  • On August 19–22, 1986, ground controllers boosted the vacant Salyut 7-Kosmos 1686 complex to a 474 km by 492 km orbit using engines on Kosmos 1686. This reduced the propellant supply of the complex to 70 kg (about 500 kg were required for controlled deorbit). In addition, Kosmos 1686 and Salyut 7 each suffered major systems breakdowns soon after they were abandoned, making the complex impossible to control.[2]
  • All previous space stations over which the Soviets maintained control were intentionally deorbited after their last cosmonaut crew departed. The Soviets estimated that the reboost gave the complex an 8-yr lifetime in orbit. They considered recovering the station using the Buran shuttle. However, following delays to and the eventual cancellation of the Buran program, Kosmos 1686 underwent uncontrolled reentry with Salyut 7 on February 7, 1991, reentering over Argentina, scattering much of its debris over the town of Capitan Bermudez.[3][4][5]

References

  1. ^ "COSMOS 1686 Satellite Details 1985-086A NORAD 16095". n2yo.com. Retrieved June 29, 2007.
  2. ^ a b c d e David S.F. Portree (1995). Mir Hardware Heritage (PDF). NASA. Archived (PDF) from the original on March 26, 2023.
  3. ^ "Spacecraft Reentry FAQ". www.aero.org. Archived from the original on May 13, 2012. Retrieved October 18, 2009.
  4. ^ Mark Wade. "Salyut 7". Encyclopedia Astronautica. Retrieved October 18, 2009.
  5. ^ John T. McQuiston (February 7, 1991). "Salyut 7, Soviet Station in Space, Falls to Earth After 9-Year Orbit". The New York Times. Retrieved October 18, 2009.