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Advanced Launch System (ALS): Electrical actuation and power systems improve operability and cost pictureTo obtain the Advanced Launch System (ALS) primary goals of reduced costs and improved operability, there must be significant reductions in the launch operations and servicing requirements relative to current vehicle designs and practices. One of the primary methods for achieving these goals is by using vehicle electrical power system and controls for all actuation and avionics requirements. A brief status review of the ALS and its associated Advanced Development Program is presented to demonstrate maturation of those technologies that will help meet the overall operability and cost goals. The electric power and actuation systems are highlighted as a specific technology ready not only to meet the stringent ALS goals (cryogenic field valves and thrust vector controls with peak power demands to 75 hp), but also those of other launch vehicles, military and civilian aircraft, lunar/Martian vehicles, and a multitude of commercial applications.
Document ID
19900011955
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sundberg, Gale R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1990
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
E-5358
NASA-TM-102547
NAS 1.15:102547
Report Number: E-5358
Report Number: NASA-TM-102547
Report Number: NAS 1.15:102547
Meeting Information
Meeting: National Aerospace and Electronics Conference
Location: Dayton, OH
Country: United States
Start Date: May 21, 1990
End Date: May 25, 1990
Sponsors: IEEE
Accession Number
90N21271
Funding Number(s)
PROJECT: RTOP 549-03-1A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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