Reduced-Mass Orbital AI Inference via Integrated Solar, Compute, and Radiator Panels
Stephen Gaalema, Samuel Indyk, and Clinton Staley

TL;DR
This paper proposes a novel satellite architecture integrating solar, radiator, and compute panels to achieve high power and compute efficiency for AI inference in space.
Contribution
It introduces a scalable, integrated satellite design with custom panels supporting high-power AI inference, improving efficiency and reducing mass.
Findings
Achieves >100 kW compute power per launched ton.
Supports 7900 simultaneous AI inferences in a full satellite.
Enables high-efficiency compute at near 40°C junction temperature.
Abstract
We describe and analyze a distributed compute architecture for SSO computational satellites that can potentially provide >100 kW compute power per launched metric ton (including deployment and station keeping mass). The architecture co-locates and integrates the solar cells, radiator, and compute functions into multiple small panels arranged in a large array. The resultant large vapor chamber radiator area per panel should permit ICs to operate at junction temperatures near 40*C with benefits in compute efficiency and reliability. Using the structure of the radiator to support the solar cells may also yield a specific power of about 500 W/kg compared to less than 100 for existing conventional implementations. Assuming development of custom solutions for all components, a 16 MW computation, 150 ton satellite comprising a 20 m x 2200 m grid of 16,000 panels can fit in a single Starship…
Peer Reviews
No public reviews on file for this paper yet. If you reviewed it on a platform where reviews are public (OpenReview, ICLR, NeurIPS, ICML), you can paste yours below so the community can read it here.
Videos
No videos yet. Explain this paper in a talk, walkthrough, or lecture? Add one.
