DocumentCode
1255714
Title
Advanced Launch System (ALS) actuation and power systems impact operability and cost
Author
Sundberg, Gale R.
Author_Institution
NASA Lewis Res. Center, Cleveland, OH, USA
Volume
5
Issue
9
fYear
1990
Firstpage
20
Lastpage
23
Abstract
A brief status review of the Advanced Launch System (ALS) is given. The use of electrical actuation integrated with a single-vehicle electrical power system and controls for all actuation and avionic requirements is highlighted. This technology will help attain the ALS primary goals of reduced costs ($300/lb Earth to LEO (low Earth orbit)) and improved operability by significantly reducing the launch operations and servicing requirements relative to current vehicle designs and practices. Six candidate government-supported programs that are involved in the relevant technologies or that could have significant applications for electric actuators and an integrated power-distribution and control system are listed with a brief explanation and description of noteworthy technology.<>
Keywords
aerospace control; aerospace instrumentation; economics; electric actuators; space vehicle power plants; NASA; US Government programs; aerospace control; costs; electrical actuation; integrated power-distribution and control system; operability; single-vehicle electrical power system; Aerospace electronics; Control systems; Costs; Electric vehicles; Low earth orbit satellites; Power system control; Power system dynamics; Power systems; Space vehicles; Valves;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems Magazine, IEEE
Publisher
ieee
ISSN
0885-8985
Type
jour
DOI
10.1109/62.59281
Filename
59281
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