Fast Auroral Snapshot Mission Unique Electronics Complete Spacecraft Electronics Contained in a Single Enclosure

The Fast Auroral Snapshot (FAST) Mission Unique Electronics (MUE), housed in a single container, controls all major spacecraft functions. The functions include, Command and Data Handling (C&DH), Attitude Control and Stabilization (ACS), battery charge control and power distribution which comprise the Power System Electronics (PSE), thermal sensing and control, pyrotechnic device firing, spacecraft health and safety functions, Instrument Data Processing Unit (IDPU) interface and Small Launch Vehicle (SLV) interface. Each of the MUE functions have been optimized to conserve mass and power, utilize packaging, mechanical hardware and electronics components that are suitable for the radiation environment in the Auroral regions. The MUE mounts on a 10 by 12 inch footprint and is 10 inches in height. It weighs 30 pounds and typically consumes less than 14 watts.

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Publication Details

Journal
FEMS Microbiology Letters
Published
2025-08-28
DOI
https://doi.org/10.26077/87kh-8434
Primary Topic
Spacecraft Design and Technology
Type
article
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article

Fast Auroral Snapshot Mission Unique Electronics Complete Spacecraft Electronics Contained in a Single Enclosure

Michael Chiville, T. Gruner, Lamar Dougherty, Jonathan Wilmot
FEMS Microbiology Letters
Spacecraft Design and Technology
article

Fast Auroral Snapshot Mission Unique Electronics Complete Spacecraft Electronics Contained in a Single Enclosure

Michael Chiville, T. Gruner, Lamar Dougherty, Jonathan Wilmot
article en

Abstract

The Fast Auroral Snapshot (FAST) Mission Unique Electronics (MUE), housed in a single container, controls all major spacecraft functions. The functions include, Command and Data Handling (C&DH), Attitude Control and Stabilization (ACS), battery charge control and power distribution which comprise the Power System Electronics (PSE), thermal sensing and control, pyrotechnic device firing, spacecraft health and safety functions, Instrument Data Processing Unit (IDPU) interface and Small Launch Vehicle (SLV) interface. Each of the MUE functions have been optimized to conserve mass and power, utilize packaging, mechanical hardware and electronics components that are suitable for the radiation environment in the Auroral regions. The MUE mounts on a 10 by 12 inch footprint and is 10 inches in height. It weighs 30 pounds and typically consumes less than 14 watts.

FEMS Microbiology LettersVol. 201(2)
Lockheed Martin (United States) (US), Goddard Space Flight Center (US)
Affordable and clean energy
Spacecraft Design and Technology
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Fast Auroral Snapshot Mission Unique Electronics Complete Spacecraft Electronics Contained in a Single Enclosure — Michael Chiville, T. Gruner, et al. · FEMS Microbiology Letters (2025) | TGRS Research Map | TGRS