Cosmos 1656

Launch Success

Liftoff Time (GMT)

14:59:00

Thursday May 30, 1985

Mission Details

Cosmos 1656

Wiki

The Tselina-2 (11F644) series of ELINT satellites were replacements for the first generation system. Based on the first generation Tselina-D ELINT, TSNII-KS at the beginning of the 1970's developed the specifications for an improved model with increased frequency range and on-board method of determining the position of fixed transmitters. The original Tselina-2 design was authorised in March 1973 and handled by prime contractor TsNIRTI Minradioprom for the ELINT equipment and KB Yuzhnoye for the spacecraft bus. The new specification for a universal Army-Navy system called for a satellite with increased mass and lifetime. This would be launched by the Zenit-2 booster, replacing the separate earlier-generation systems. Data transmission was directly to ground stations via geosynchronous communications satellites. Delays in development of the Zenit-2 launch vehicle resulted in launching the first two trials flights by Proton-K Blok-DM-2 booster in 1984 and 1985. Tselina-2 is 3-axis stabilized with addition of a gravity gardient boom, basicly an enlarged version of the Tselina-D bus.

Low Earth Orbit

1 Payload

3,200 kilograms

Rocket

Retired
Proton K/Block-DM-2

Active 1982 to 2012

Khrunichev State Research and Production Space Center logo

Manufacturer

Khrunichev

Rocket

Height: 57.64m

Payload to Orbit

LEO: 19,000 kg

GTO: 2,400 kg

Liftoff Thrust

9,548 Kilonewtons

Fairing

Diameter: 4.35m

Height: 10.4m

Stages

4

Launch Site

Site 200/40

Baikonur Cosmodrome, Kazakhstan

Fastest Turnaround

26 days 14 hours

Stats

Proton-K


127th

Mission

5th

Mission of 1985

Khrunichev State Research and Production Space Center


1904th

Mission

35th

Mission of 1985

1985


43rd

Orbital launch attempt