Manufacturer | ISRO |
---|---|
Country of origin | India |
Operator | ISRO |
Applications | Gamma ray astronomy |
Specifications | |
Launch mass | 106–150 kilograms (234–331 lb) |
Power | ~100 watts |
Batteries | Ni-Cd |
Equipment | Gamma-Ray Burst Retarded Potential Analyser[ citation needed ] |
Regime | Low Earth |
Design life | 2 years |
Dimensions | |
Production | |
Status | Retired |
Built | 4 |
Launched | 4 |
Retired | 1 |
Lost | 3 |
Maiden launch | SROSS-A/SROSS-1 24 March 1987 |
Last launch | SROSS-C2 4 May 1994 |
Related spacecraft | |
Derived from | Rohini |
The Stretched Rohini Satellite Series (SROSS) are a series of satellites developed by the Indian Space Research Organisation as follow ons to the Rohini Satellites [1] for conducting astrophysics, Earth Remote Sensing, and upper atmospheric monitoring experiments as well as for new and novel application-oriented missions. [2] These satellites were the payload of the developmental flights of the Augmented Satellite Launch Vehicle. [1]
The first two satellites in the series did not make it into orbit due to launch vehicle failure. SROSS-A carried two retro-reflectors for laser tracking. [1] SROSS-B carried two instruments; a West German Monocular Electro Optical Stereo Scanner (MEOSS) and ISRO's 20-3000keV Gamma-ray Burst Experiment (GRB). [1]
The third, SROSS 3 (also known as SROSS C), attained a lower-than-planned orbit on 20 May 1992. The GRB monitored celestial gamma ray bursts in the energy range 20–3000 keV. SROSS C and C2 carried a gamma-ray burst (GRB) experiment and a Retarded Potential Analyzer (RPA) experiment. The GRB experiment operated from 25 May 1992 until reentry on 14 July 1992. The instrument consisted of a main and a redundant CsI(Na) scintillator operating in the energy range 20–3000 keV. The crystals were 76 mm (main) and 37 mm (redundant) in diameter. Each had a thickness of 12.5 mm. A 'burst mode' was triggered by the 100–1024 keV count rate exceeding a preset limit during a 256 or 1024 ms time integration. In this mode, 65 s of temporal and 2 s of spectral data prior to the trigger are stored, as well as the subsequent 16 s of spectral data and 204 s of temporal data. The low resolution data consists of two energy channels (20–100 keV and 100–1024 keV) from 65 s before the trigger to 204 s after the trigger in 256 ms integrations. The 20–1024 keV rates are also recorded with a 2 ms resolution for 1 s prior to 1 s after trigger and a 16 ms resolution for 1s prior to 8 s after the trigger. Energy spectra are conducted with a 124 channel PHA. Four pre-trigger spectra and 32 post-trigger spectra are recorded for every burst with a 512 ms integration time. [3] The RPA measured temperature, density and characteristics of electrons in the Earth's ionosphere. [1] The GRB experiment computer system used the RCA CDP1802 microprocessor. [4]
SROSS-C2 was launched on 4 May 1994. The gamma ray burst experiments on board SROSS-C2 are an improved version of the GRB payload flown successfully on the SROSS-C satellite. The improvements include enhancements of the on-board memory and a better measurement of the background spectra after a burst event. These improvements led to the discovery of twelve candidate events detected up to 15 February 1995, out of a total of 993 triggers. [3] The SROSS-C2 spacecraft is one of the satellites included in the Interplanetary Network [5] The SROSS C2 satellite also used an RCA CDP1802 microprocessor for the GRB experiment. [6]
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