NASA NTRS · 19790009722
The 25 W power module evolution study. Part 3: Conceptual designs for power module evolution. Volume 5: Mission accommodations
Abstract
The capability of the 25 kW power module to conduct representative missions which include Earth, solar, and stellar observation as well as zero-gravity experiments was assessed. Mission accommodations and related technical characteristics of the various operating modes are summarized. The minimum power module provides a substantial mission support on sortie flights. The addition of an attitude sensor is required for free-flying pointing missions.
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1979-01-27. The 25 W power module evolution study. Part 3: Conceptual designs for power module evolution. Volume 5: Mission accommodations. https://ntrs.nasa.gov/citations/19790009722
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