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Salient Features |
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Physical |
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Shape |
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Sphere-cone-flare |
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Overall size |
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Base diameter : 2.03 m
Height : 1.67 m |
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Mass at launch |
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555 kg |
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Thermal protection |
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Ablative Nose Cap
Re-usable Silica TPS
Low Density Ablatives |
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Navigation, Guidance
and Control |
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Processing |
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Mission Management Unit (MMU)
Inertial Measurement Unit (IMU)
Sun sensors, Magnetometer Sensors |
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Actuators |
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Magnetic Torquer/22N thrusters |
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Propulsion |
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22 N Bi-propellant thrusters (eight nos.) |
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Power |
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Battery and body mounted solar panels |
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TTC |
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S-Band with Belt Array antenna |
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Deceleration system |
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Three stage parachute system |
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Experiments: |
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1. Growth of Ico Ga-Mg-Zn quasi crystal |
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2. Bio-mimetic synthesis of inorganic material |
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Launcher |
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PSLV-C7 with CARTOSAT-2, LAPAN-TUBSAT
and PEHUENSAT-1 as co-passengers |
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Orbit |
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635 km circular (polar orbit) |
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No. of days in orbit |
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12 |
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Impact velocity |
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12 m/s |
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Recovery |
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140 km off Sriharikota in the Bay of Bengal |
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Recovery aids |
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Flotation system UHF Beacon and Sea Marker Dye |
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Recovery team |
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Indian Coast Guard assisted by Indian Navy |