NASA/JPL · Aerospace · 2018
Interior Exploration using Seismic Investigations, Geodesy and Heat Transport. Stationary Mars lander built on the Phoenix design with larger solar panels. Equipped with a robotic instrument deployment arm that placed a French-built seismometer (SEIS) and a German-built self-hammering heat probe (HP3 'mole') on the surface. Detected over 1,300 marsquakes and revealed Mars's interior structure befo
| Category | Aerospace |
| Status | Active |
| Year | 2018 |
| Origin | USA |
| Height | 1000 mm |
| Weight | 358 kg |
| Payload | 9 kg |
| Degrees of freedom | 4 |
| Battery | 25 Ah |
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