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Power Extension Package (PEP) system definition extension, orbital service module systems analysis study. Volume 1: Executive summaryAn array deployment assembly, power regulation and control assembly, the necessary interface, and display and control equipment comprise the power extension package (PEP) which is designed to provide increased power and duration, as well as reduce fuel cell cryogen consumption during Spacelab missions. Compatible with all currently defined missions and payloads, PEP imposes minimal weight and volume penalties on sortie missions, and can be installed and removed as needed at the launch site within the normal Orbiter turnaround cycle. The technology on which it is based consists of a modified solar electric propulsion array, standard design regulator and control equipment, and a minimally modified Orbiter design. The requirements from which PEP was derived, and the system and its performance capabilities are described. Features of the recommended project are presented.
Document ID
19790025066
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
August 1, 1979
Subject Category
Space Transportation
Report/Patent Number
MDC-G7870-VOL-1
NASA-CR-160321
Report Number: MDC-G7870-VOL-1
Report Number: NASA-CR-160321
Accession Number
79N33237
Funding Number(s)
CONTRACT_GRANT: NAS9-15532
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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