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Information courtesy of EADS Astrium.
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For more details of how the instruments fit in the lander
see the lander
interior section»
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Key::::::::: |
| 1 |
Spin Up & Eject Mechanism |
| 2 |
Thermal Protection |
| 3 |
Pilot chute and deployment device |
| 4 |
HEPA filter |
| 5 |
Stowed main parachute |
| 6 |
Stowed airbags |
| 7 |
Stowed lander |
| 8 |
Airbag gassing system |
| 9 |
Front shield structure |
| 10 |
Thermal protection |
| 11 |
Solar absorber |
| 12 |
Gas Analysis Package |
| 13 |
PAW |
| 14 |
Robotic arm |
| 15 |
Electronics |
| 16 |
Battery |
| 17 |
Transceiver |
| 18 |
Lander base |
| 19 |
Main hinger |
| 20 |
Solar panel hinge |
| 21 |
Antenna |
| 22 |
Lid structure |
| 23 |
Solar Cells |
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