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| Attribute | ||
|---|---|---|
| Operator | Blue Origin | Astrobotic |
| Prime contractor | Blue Origin | Astrobotic |
| Status | In development | Lost |
| Customer | NASA-CLPS | NASA-CLPS |
| Launch date | 2026-07 (NET) | 2024-01-08 |
| Landing date | — | — |
| Landing site | Lunar south pole region | Sinus Viscositatis (planned; never reached) |
| Payload | 3,000 kg surface payload capacity (21,350 kg wet lander mass) (2026-05-28) | 20 payloads from 7 nations (2024-01-08) |
| Contract value | — | $108M (2024-01-08) |
| 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. | 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. |
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Underlying dataset: GET /api/moon/landers. Methodology: /moon/methodology.