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New technologies for space avionicsThis report reviews a 1994 effort that continued 1993 investigations into issues associated with the definition of requirements, with the practice concurrent engineering and rapid prototyping in the context of the development of a prototyping of a next-generation reaction jet driver controller. This report discusses lessons learned, the testing of the current prototype, the details of the current design, and the nature and performance of a mathematical model of the life cycle of a pilot operated valve solenoid.
Document ID
19950011781
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Aibel, David W.
(Lockheed Sanders, Inc. Nashua, NH, United States)
Dingus, Peter
(Lockheed Sanders, Inc. Nashua, NH, United States)
Lanciault, Mark
(Lockheed Sanders, Inc. Nashua, NH, United States)
Hurdlebrink, Debra
(Lockheed Sanders, Inc. Nashua, NH, United States)
Gurevich, Inna
(Lockheed Sanders, Inc. Nashua, NH, United States)
Wenglar, Lydia
(Lockheed Sanders, Inc. Nashua, NH, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1994
Subject Category
Spacecraft Instrumentation
Report/Patent Number
NASA-CR-197574
NAS 1.26:197574
Report Number: NASA-CR-197574
Report Number: NAS 1.26:197574
Accession Number
95N18196
Funding Number(s)
CONTRACT_GRANT: NAS9-18873
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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