Gram-Scale ChipSat Spacecraft for Light Sailing in LEO

Cornell University’s Alpha mission is a 1U CubeSat that deploys a retroreflective free-flying light sail in LEO. Mounted to the sail, and serving as its flight computers, are four ChipSats –gram-scale spacecraft assembled onto a single palm-sized PCB. These satellites collect and downlink data on the sail’s orbital position and attitude kinematics, communicating directly with low-cost ground stations around the globe. This paper introduces the ChipSat developed specifically for the Alpha mission launching in 2025. The new femto-satellite builds on previous-generation designs with a significant revamp of the RF communications. This paper provides an overview of the as-flown ChipSat design and outlines significant test milestones that validated it for flight. Light sail integration, flight software architecture, and the ground segment are also discussed.

Publication Details

Journal
Digital Commons - USU (Utah State University)
Published
2025-08-04
DOI
https://doi.org/10.26077/d403-5c25
Primary Topic
Spacecraft Dynamics and Control
Type
article
Field-Weighted Citation Impact
0.00
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article

Gram-Scale ChipSat Spacecraft for Light Sailing in LEO

Digital Commons - USU (Utah State University)
Spacecraft Dynamics and Control
article

Gram-Scale ChipSat Spacecraft for Light Sailing in LEO

article en

Abstract

Cornell University’s Alpha mission is a 1U CubeSat that deploys a retroreflective free-flying light sail in LEO. Mounted to the sail, and serving as its flight computers, are four ChipSats –gram-scale spacecraft assembled onto a single palm-sized PCB. These satellites collect and downlink data on the sail’s orbital position and attitude kinematics, communicating directly with low-cost ground stations around the globe. This paper introduces the ChipSat developed specifically for the Alpha mission launching in 2025. The new femto-satellite builds on previous-generation designs with a significant revamp of the RF communications. This paper provides an overview of the as-flown ChipSat design and outlines significant test milestones that validated it for flight. Light sail integration, flight software architecture, and the ground segment are also discussed.

Digital Commons - USU (Utah State University)
Openalex Percentile: Top 47%
Spacecraft Dynamics and Control
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