NEXT SPACEFLIGHT

Status

Failure

Yantar-4KS1 n°100

Launch Time
Sat Jul 09, 1988 13:25 UTC

Rocket

Soyuz U
RVSN USSR
Status: Retired
Price: $20.0 million
Liftoff Thrust: 4,456 kN
Payload to LEO: 6,860 kg
Payload to GTO: 0 kg
Stages: 3
Strap-ons: 4
Rocket Height: 51.32 m
Fairing Diameter: 3.0 m
Fairing Height: 15.59 m

Mission Details

Yantar-4KS1 n°100

Yantar satellites are more accurate ground observation satellites than the Zenit satellites previously used. The big innovation compared to the Zenit satellites is the compartment for the return of photographic film, which is no longer shaped like a sphere but like a cone.

Yantar-2K have a big advantage, which even the American KH-7 does not have, because it will be equipped with two small capsules (SK) that will allow to return films to Earth without waiting for the end of the satellite mission. In addition, the camera and on-board computer will be reusable. The Yantar-2K will also be equipped with the new Kondor orientation control system, developed by KF TsKBEM.

The different versions of the satellites are called Yantar-xK, the letter K designating the manufacturer Kuybichev who designed and built these satellites. The Yantar-2K satellites are nicknamed Feniks, the Yantar-1KFT Kometa and the Yantar-4K Kobalt.

It should be noted that the Yantar-4KS1M are not recoverable, and transmit their pictures directly from orbit, thus reducing the time between the taking of pictures and their acquisition by the Soviet armed forces.

Payloads: 1
Total Mass: 6,600.0 kg
Low Earth Orbit

Location

Site 1/5, Baikonur Cosmodrome, Kazakhstan

Stats

1988

60th orbital launch attempt

Soyuz U

541st mission
23rd mission of 1988
13th failed mission