Small commercial lunar lander (Series 1) designed and built by ispace for low-cost, high-frequency delivery of customer payloads to the lunar surface; used for HAKUTO-R Mission 1.
Delta V (m/s)
Not publicly disclosed
Payload Capacity (kg)
30
| Specification | Value |
|---|---|
| Delta V (m/s) | Not publicly disclosed |
| Dry Mass (kg) | 340 |
| Crew Capacity | 0 |
| Landing Precision M | Not publicly disclosed |
| Payload Capacity (kg) | 30 |
| Mission Duration (days) | 135 |