LunaCube Spacecraft

LunaCube
Satellite LunaCube
Type CubeSat
Units or mass 6U
Organization University of Tokyo
Institution University
Entity Academic / Education
Nation Japan
Partners University of Houston, Chubu University, University of Fukui
Oneliner

Dual-satellite lunar navigation system technology demonstration.

Description

"The LunaCube is a dual-satellite lunar navigation system that employs the multi-epoch doubledifferenced pseudorange observation (MDPO) algorithm. The MDPO process involves collecting pseudorange measurements between two lunar orbiters and both the user and surface reference receivers. 

Through the double-difference observation process, the influences of satellite orbit determination (OD) errors and satellite clock offset on user positioning accuracy are significantly eliminated. This reduces the reliance on high-standard onboard clocks that require high power. 

Consequently, it enables the use of small-sized satellites, achieving a 50-meter user positioning accuracy with just a one-minute observation by placing two 6U satellites in a low lunar orbit (LLO)."

Sources [1]
Photo sources [1]
Keywords Propulsion

Related Spacecraft

Spacecraft Status Launcher Date Orbit
LunaCube A (Lunar Navigation CubeSat) not launched not launched 2026-12-30 Moon
LunaCube B (Lunar Navigation CubeSat) not launched not launched 2026-12-30 Moon

Last modified: 2024-12-28

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Created by Erik Kulu

Email: erik.kulu@nanosats.eu
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