Corsa A

Launch Failure

Liftoff Time (GMT)

06:00:00

Wednesday February 4, 1976

Mission Details

Launch Notes

Unknown failure.

Corsa A

Wiki

The spacecraft Corsa (Cosmic Radiation Satellite) had the shape of an octagonal prism, with a maximum width of 80 cm and height of 65 cm, and was spin-stabilized at a rate of 5 to 8 rpm. The spin axis was maneuvered by means of magnetic torquing. Eleven X-ray detectors of various specifications were devoted to the observation of cosmic X-rays. Four detectors had fields of view perpendicular to the spin axis and scanned over a wide region of the sky in search of X-ray novae and transients. The other seven detectors had FOVs along the spin axis and were used to study selected celestial objects. Observational data could either be telemetered back in real-time or stored in an onboard data recorder. Telemetry frequencies were 136.725 MHz at 500 mW and 400.450 MHz at 100 mW.

Low Earth Orbit

1 Payload

85 kilograms

Rocket

Retired
Mu-III C

Active 1974 to 1979

Institute of Space and Aeronautical Science logo

Agency

ISAS

Payload to Orbit

LEO: 195 kg

Stages

3

Strap-ons

8

Launch Site

Mu Pad

Uchinoura Space Center, Japan

Fastest Turnaround

143 days 23 hours

Stats

Mu-III


3rd

Mission

1st

Mission of 1976

Institute of Space and Aeronautical Science


7th

Mission

1st

Mission of 1976

1976


12th

Orbital launch attempt