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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 second ispace mission will perform a soft landing and deploy a rover for surface exploration and data collection on the Moon.

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) ispace rover

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 August 2022

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