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| Attribute | HAKUTO-R Series 2 Resilience (SMBC × HAKUTO-R Venture Moon) Trust: Agency-primary Last verified Remove × | |
|---|---|---|
| Operator | Astrobotic | ispace |
| Prime contractor | Astrobotic | ispace |
| Status | Lost | Lost |
| Customer | NASA-CLPS | private |
| Launch date | 2024-01-08 | 2025-01-15 |
| Landing date | — | 2025-06-05 |
| Landing site | Sinus Viscositatis (planned; never reached) | Mare Frigoris (center; hard landing) |
| Payload | 20 payloads from 7 nations (2024-01-08) | Tenacious micro-rover (5 kg, ispace EU) + 5 commercial payloads (2025-06-05) |
| Contract value | $108M (2024-01-08) | — |
| Outcome | Maiden flight of ULA's Vulcan Centaur. Helium pressurant valve failed to reseal post-actuation, over-pressurizing the oxidizer tank and rupturing it. Lander commanded into controlled re-entry; burned up over South Pacific 2024-01-18. | Laser Range Finder anomaly during descent caused hard landing; data lost ~90 seconds before scheduled touchdown at 19:17 UTC. NASA's LRO imaged impact dark-smudge on 2025-06-11. ispace's 2025-06-24 technical analysis ruled out propulsion/power; isolated cause to LRF. |
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Underlying dataset: GET /api/moon/landers. Methodology: /moon/methodology.