NEXT SPACEFLIGHT

Status

Failure

Tsikada n°3

Launch Time
Tue Nov 29, 1977 07:05 UTC

The launch was a failure due to a malfunction on the second stage S5.23 engine.

Rocket

Cosmos-3M
Image Credit: OKB-586
RVSN USSR
Status: Retired
Liftoff Thrust: 1,486 kN
Payload to LEO: 1,500 kg
Payload to GTO: 0 kg
Stages: 2
Strap-ons: 0
Rocket Height: 32.42 m
Fairing Diameter: 2.44 m
Fairing Height: 5.72 m

Mission Details

Tsikada n°3

Tsikada was a Soviet civilian satellite navigation system used by the Soviet Merchant Marine and Academy of Sciences, but also by the military. It was equivalent to the purely military Parus system.

The Tsikada satellites were very similar to the Parus satellites and also used an NPO PM-built pressurized cylindrical bus with gravity-gradient stabilization. The satellites transmitted Doppler-shifted VHF transmissions at around 150 MHz and 400 MHz of their position and orbital characteristics. They operated from a 1000 km orbit with 82.9° inclination. Satellites were placed in planes spaced 45° apart.

The development of Tsikada began in 1974 and the first satellite was launched in 1976. The system entered the operational phase in 1978.

Also operated in the Tsikada system were the Nadezhda and Nadezhda-M satellites, which featured an additional search and rescue system for locating vessels and aircraft in distress. Beginning in the 1990ies, the Tsikada system was gradually superseded by the Uragan (GLONASS) system.

Payloads: 1
Total Mass: 820.0 kg
Low Earth Orbit

Location

Site 132/1, Plesetsk Cosmodrome, Russia

Stats

1977

115th orbital launch attempt

Cosmos-3

191st mission
25th mission of 1977
15th failed mission