IS Mockup

Launch Success

Liftoff Time (GMT)

10:59:00

Saturday November 1, 1969

Mission Details

Launch Notes

Suborbital test flight.

IS Mockup

Wiki

IS is a family of Soviet military satellites developed in the 1960s with the capability to destroy enemy reconnaissance satellites in low orbit. The program, after being declared operational in 1973, was abandoned in 1993. The IS satellite is a kamikaze-type satellite that carries a conventional explosive charge that it detonates at a short distance from the targeted satellite after carrying out a series of maneuvers to get close to it. The IS satellite has a mass of 2 450 kg and consists of two subassemblies: the first contains the guidance system and a 300 kg explosive charge, the second part contains the propulsion system. The body of the satellite is designed to fragment under the effect of the explosion into 12 groups of shrapnel to ensure the destruction of a target within a radius of 1 km. However, a frontal interception allows destruction only at a distance of 400 meters while an explosion intervening while the satellite catches up with its target allows its destruction at a distance of 2 km. The rocket engine can be reignited a large number of times and is designed to operate cumulatively for 300 seconds. The IS satellite must be placed on the same orbit as the target in order to destroy it. This can be achieved twice a day when the launcher can place the IS satellite on the same orbital plane as its target. Once launched, the satellite is guided by ground controllers to catch up with the target in 1 to 2 orbits. The IS satellite's radar then takes over to provide guidance until the target is only a few tens of meters away. The explosive charge is then triggered, which ejects shrapnel that damages the targeted satellite.

Suborbital

1 Payload

2,450 kilograms

Rocket

Retired
Tsyklon-2

Active 1969 to 2006

Yuzhmash logo

Manufacturer

Yuzhmash

Rocket

Height: 39.65m

Payload to Orbit

LEO: 2,850 kg

GTO: 0 kg

Liftoff Thrust

2,650 Kilonewtons

Fairing

Diameter: 3m

Height: 10.7m

Stages

2

Launch Site

Site 90/20

Baikonur Cosmodrome, Kazakhstan

Fastest Turnaround

47 hr 23 min

Stats

Tsyklon-2


2nd

Mission

2nd

Mission of 1969

Yuzhmash


445th

Mission

71st

Mission of 1969