Spacecraft data:
Prime manufacturer | ISRO |
Platform | I-2K (I-2000) Bus |
Operator | Insat |
Mass at launch | 1982 kg |
Dry Mass | kg |
Basic shape | |
Dimension (m) | 2.0 x 2.0 x 3.6 m |
Equipment | 6 Ku-band, 6 ext. C-band transponders, Ka-band beacons |
Solar array | 2 deployable solar arrays |
Antennae | One 2m and one 2.2 m single shell shaped reflector Antennae (transmit and receive) |
Stabilization | |
Propulsion | Bi propellant-Mono Methyl Hydrazine and Mixed Oxides of Nitrogen (MON-3) |
DC power | 2600 W |
Design lifetime | 12 yrs |
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 GSAT-14 Photo Credit: ISRO
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