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| Attribute | HAKUTO-R Series 2 Resilience (SMBC × HAKUTO-R Venture Moon) Trust: Agency-primary Last verified Remove × | |
|---|---|---|
| Operator | Blue Origin | ispace |
| Prime contractor | Blue Origin | ispace |
| Status | In development | Lost |
| Customer | NASA-CLPS | private |
| Launch date | 2026-07 (NET) | 2025-01-15 |
| Landing date | — | 2025-06-05 |
| Landing site | Lunar south pole region | Mare Frigoris (center; hard landing) |
| Payload | 3,000 kg surface payload capacity (21,350 kg wet lander mass) (2026-05-28) | Tenacious micro-rover (5 kg, ispace EU) + 5 commercial payloads (2025-06-05) |
| Contract value | — | — |
| Outcome | First flight test of Blue Moon Mark 1. Carries NASA CLPS Stereo Cameras for Lunar Plume-Surface Studies + Laser Retroreflective Array. Targets 100 m landing precision. Lander completed full-scale thermal-vacuum testing at NASA Plum Brook (Armstrong Test Facility) May 2026. | 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.