IRS P2

IRS P2

First Spacecraft successfully orbited onboard the second developmental flight of PSLV. Mission completed during 1997 after serving for 3 years.

Mission Operational Remote Sensing
Weight 804 kg
onboard power 510 Watts
Communication S-band, X-band
Stabilization Three axis body stabilized with 4 Reaction Wheels, Magnetic torquers
RCS 4 tanks containing Monopropellant Hydrazine based with sixteen 1 N thrusters and one 11 N thruster
Payload Two solid state Push Broom Cameras operating in four spectral bands in the visible and near-IR range using CCD arrays: LlSS-2A & LlSS-2B (Resolution: 32.74 metre)
Launch date October 15, 1994
Launch site Monopropellant Hydrazine based with sixteen 1 N thrusters & one 11N thrusters
Launch vehicle PSLV-D2
Inclination 98.68 Degree
Repetivity 24 days
Mission Completed 1997

IRS P2