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SpaceRadar | Lander Details

HAKUTO-R

PAYLOAD CAPACITY - TLI (Trans Lunar Injection)

X band for lander-Earth uplink and downlink. Wi-Fi and sub-Ghz communications between mobile payloads and lander.

PAYLOAD CAPACITY - TO ORBIT

30 kg

The first ispace mission will perform a soft landing on the Moon. This will be the first privately-led Japanese mission to land on the lunar surface.

60 kg

104 X 36.7 X 60.2 cm (per bay, 2 bays available)

3.0 W/kg, 28 VDC unregulated & 12 V, 5V regulated

1) Rashid lunar rover by the Mohammed bin Rashid Space Centre (MBRSC)
2) Solid-state battery test module by NGK Spark Plug
3) Transformable lunar robot by the Japan Aerospace Exploration Agency (JAXA)
4) AI flight computer by Mission Control Space Services, which will collaborate with the Rashid rover
5) Multiple cameras by Canadensys
6) Panels engraved with the names of HAKUTO crowdfunding supporters

The duration of nominal surface operations is 12 sunlit days

0 (Partner with Draper Laboratory in their CLPS mission. Not eligible to be Main Contractors yet)

PAYLOAD CAPACITY - TO SURFACE

PAYLOAD SIZE

POWER DISTRIBUTION (FOR PAYLOAD)

COST

COMMUNICATIONS AVAILABLE

MISSION PLAN

SHIP MANIFEST

MISSION OBJECTIVES

EXPECTED DURATION

FIRST AWARDED CLPS CONTRACT

TOTAL CLPS CONTRACT

Last Updated on November 2023

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