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Analysis of the Artemis I Orion Spacecraft Power System PerformanceNASA successfully completed an uncrewed test flight of the Orion spacecraft during the 26-day Artemis I mission in November and December 2022. The Artemis I mission profile included several potentially stressing features for Orion electrical power system (EPS) performance, including eclipse duration, multiple propulsive or navigational maneuvers which constrained positioning of the solar array wings (SAWs), and the proximity and phasing of various events together. All of these features vary significantly with Earth-sun-moon geometry, providing a unique challenge for predicting EPS performance before an exact launch date is known.

This presentation will provide a brief mission overview, discuss the different computer models with varying levels of fidelity used to analyze Orion EPS performance, as well as the screening process developed to incorporate EPS performance as a consideration for launch epoch selection. Final preflight model predictions of EPS performance will be compared to in-flight telemetry measurements, and several EPS anomalies observed will be briefly discussed.
Document ID
20230004171
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Spencer Furin
(Glenn Research Center Cleveland, Ohio, United States)
Hector Hernandez
(Johnson Space Center Houston, Texas, United States)
Anuj Patel
(Lockheed Martin (United States) Bethesda, Maryland, United States)
Date Acquired
March 29, 2023
Subject Category
Electronics and Electrical Engineering
Spacecraft Propulsion and Power
Meeting Information
Meeting: 40th Annual Space Power Workshop
Location: Torrance, CA
Country: US
Start Date: April 25, 2023
End Date: April 27, 2023
Sponsors: The Aerospace Corporation
Funding Number(s)
WBS: 374409.06.90.03
CONTRACT_GRANT: NNJ06TA25C
WBS: 573754.01.01.01.18.05
WBS: 374409.06.90.10.01
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Peer Committee
Keywords
Orion
MPCV
EPS
Electrical Power System
Spacecraft Power
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