GSat 4 [ISRO] |
GSAT-4 is envisaged as a technology demonstrator. The communication payload consists of multi-beam Ka-band bent pipe and regenerative transponder and navigation payload in C-band, L1 and L5 bands. GSAT-4 employs several new technologies like bus management unit, miniaturised dynamically tuned gyros, lithium-ion battery, 70 Volt bus for Ka-band TWTAs and electric propulsion. GSAT-4 also incorporates technological experiments like on-board structural dynamic experiment, thermal control coating experiment and vibration beam accelerometer. With a lift-off mass of about 2180 kg, the spacecraft generates 276 W of power in summer solstice.
It features a piggyback astronomical payload, the israeli TAUVEX -2 (Tel Aviv
University Ultra Violet Explorer), which was originally slated to fly on the Spektr-RG spacecraft. TAUVEX is mounted on a rotating table
on the east surface of GSat 4. It is operated in a scanning mode. The TAUVEX-II payload
comprising three Ultra-Violet band telescopes developed by Tel Aviv University and Israel
space agency, ELOP, for surveying a large part of the sky in the 1400-3200 Å wavelength.
| Nation: | India |
|---|---|
| Type / Application: | Experimental Communication, x-ray astronomy |
| Operator: | ISRO |
| Contractors: | ISRO |
| Equipment: | Ka-band transponders, TAUVEX-2 |
| Configuration: | I-2K (I-2000) Bus |
| Propulsion: | LAM |
| Lifetime: | |
| Mass: | 2180 kg |
| Orbit: | GEO |
| Satellite | Date | LS | Launcher | Remarks: | |
|---|---|---|---|---|---|
| GSat 4 (HealthSat) | 2010 | Sr | GSLV Mk.2 |
Further GSat missions:
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Source: ISRO Website
Last update: 27.09.2009
Contact: gunter.krebs@skyrocket.de
© Gunter Dirk Krebs