Gamma (satellite)

Gamma
Operator RKA
COSPAR ID 1990-058A
SATCAT № 20683
Mission duration 2 years
Start of mission
Launch date July 11, 1990 (1990-07-11)
Rocket Soyuz[1]
Launch site Tyuratam
End of mission
Decay date February 28, 1992 (1992-02-28)
Orbital parameters
Eccentricity 0.00326
Perigee 190 km [1]
Apogee 233 km [1]
Inclination 51.6°
Period 88.45  min
Main
Wavelengths Gamma ray
Instruments
Gamma-1 telescope (50 MeV to 6 GeV)[2]
Disk-M telescope (20 keV to 5 MeV)[2]
Pulsar X-2 telescope (2-25 keV)[2]

Gamma was a Soviet gamma ray telescope. It was launched on 11 July 1990 into an orbit around Earth with a height of 375 km and an inclination of 51.6 degrees. It lasted for around 2 years. On board the mission were three telescopes, all of which could be pointed at the same source. The project was a joint Soviet-French project.[2]

Background

Drawing of the Gamma space telescope satellite. The spaceframe and subsystems of the satellite were based on the Progress spacecraft.

The Gamma-1 telescope was the main telescope. It consisted of 2 scintillation counters and a gas Cerenkov counter. With an effective area of around 0.2 square metres (2.2 sq ft), it operated in the energy range of 50 MeV to 6 GeV. At 100 MeV it initially had an angular resolution of 1.5 degrees, with a field of view of 5 degrees and an energy resolution of 12%. A Telezvezda star tracker increased the pointing position accuracy of the Gamma-1 telescope to 2 arcminutes by tracking stars up to an apparent magnitude of 5 within its 6 by 6 degree field of view. However, due to the failure of power to a spark chamber, for most of the mission the resolution was around 10 degrees.[2]

The telescope was conceived in 1965, as part of the Soviet Cloud Space Station, which evolved into the Multi-module Orbital Complex (MOK).[3] When work on Gamma finally began in 1972, it was intended to create a Gamma observatory, the first space station module for MOK, the first modular space station in the Salyut programme.[4] For this, it was designed to add the scientific instruments of the observatory to a spacecraft derived from the Progress spacecraft – with the Progress in turn being a Soyuz spacecraft derivate – and that this spacecraft would dock to a MOK space station. However, in 1974, at the time it became a joint venture with France, the MOK space station project was canceled, and in February 1976, the Soviet space program was reconfigured. When on 16 February 1979 production of the telescope was authorized, the plans for the Soviet space station modules had evolved to use the Functional Cargo Block of the TKS spacecraft instead, with the Kvant-1 Roentgen observatory eventually becoming the first such module for Mir – as a result of these changes the Gamma observatory was redesigned as the free flying Gamma satellite. At that time the telescope was authorized in 1979, it was planned to be launched in 1984, but the actual launch was delayed until 1990.

Operation

The Disk-M telescope operated in the energy range 20 keV - 5 MeV. It consisted of Sodium iodide scintillation crystals, and had an angular resolution of 25 arcminutes. However, it stopped working shortly after the mission was launched.[2]

Finally, the Pulsar X-2 telescope had 30 arcminute resolution and a 10 deg x 10 deg field of view, and operated in the energy range 2-25 keV.[2]

Observations included studies of the Vela Pulsar, the Galactic Centre, Cygnus X-1, Hercules X-1 and the Crab Nebula. The telescopes also measured the Sun during peak solar activity.[2]

References

Wikimedia Commons has media related to Gamma (satellite).
  1. 1 2 3 "NASA - NSSDCA - Spacecraft - Trajectory Details". nssdc.gsfc.nasa.gov. NASA. Retrieved 22 April 2016.
  2. 1 2 3 4 5 6 7 8 "The Gamma Satellite". NASA. Retrieved 2008-03-01.
  3. ↑ "Gamma". Astronautix.com. Retrieved 2008-03-02.
  4. ↑ Portree, David (March 1995). "Mir Hardware Heritage" (PDF). NASA. Retrieved 24 August 2012.
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