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 Full-size model of Hakuto-R | |
| Mission type | Lunar landing, technology demonstration |
|---|---|
| Operator | ispace |
| COSPAR ID | 2025-010B |
| SATCAT no. | 62717 |
| Website | ispace-inc |
| Mission duration | 1 month and 11 days (elapsed) |
| Spacecraft properties | |
| Spacecraft | Hakuto-R Resilience |
| Spacecraft type | Lunar lander |
| Manufacturer | ispace |
| Landing mass | 340 kg (750 lb) |
| Dimensions | Width: 2.5 m (8 ft 2 in) Height: 2.3 m (7 ft 7 in) |
| Start of mission | |
| Launch date | 15 January 2025, 06:11:39 UTC (1:11:39 am EST) |
| Rocket | Falcon 9 Block 5 (B1085.5), Flight 425 |
| Launch site | Kennedy, LC-39A |
| Contractor | SpaceX |
| Resilience Lunar lander | |
| Landing date | NET April 2025 (planned)[1] |
| Landing site | Mare Frigoris (60°30′N 4°36′W / 60.5°N 4.6°W)[1] |
| Tenacious Lunar rover | |
| Landing date | NET April 2025 (planned)[1] |
| Landing site | Mare Frigoris (60°30′N 4°36′W / 60.5°N 4.6°W)[1] |
Hakuto-R Mission 2 is a robotic lunar landing mission launched on 15 January 2025 at 06:11:39 UTC (1:11:39 am EST, local time at the launch site). Developed by ispace, the lander will deliver a new micro rover manufactured by the company, as well as other payloads. Like Hakuto-R Mission 1, this mission will serve as a technology demonstration, with the final goal of providing reliable transportation and data services on the Moon. The lander is named Resilience.[2]
- ^ a b c d "ispace Announces SMBC x HAKUTO-R Mission 2 Venture Moon Mission Milestones & Ventures". ispace, Inc. 18 December 2024. Retrieved 12 January 2025.
- ^ "ispace Announces Mission 2 with Unveiling of Micro Rover Design". ispace. Retrieved 22 June 2024.