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Conceptual design study for an advanced cab and visual system, volume 2The performance, design, construction and testing requirements are defined for developing an advanced cab and visual system. The rotorcraft system integration simulator is composed of the advanced cab and visual system and the rotorcraft system motion generator, and is part of an existing simulation facility. User's applications for the simulator include rotorcraft design development, product improvement, threat assessment, and accident investigation.
Document ID
19820017391
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rue, R. J. (Boeing Military Airplane Development Wichita, KS, United States)
Cyrus, M. L. (Boeing Military Airplane Development Wichita, KS, United States)
Garnett, T. A. (Boeing Military Airplane Development Wichita, KS, United States)
Nachbor, J. W. (Boeing Military Airplane Development Wichita, KS, United States)
Seery, J. A. (Boeing Military Airplane Development Wichita, KS, United States)
Starr, R. L. (Boeing Military Airplane Development Wichita, KS, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1980
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-166236
NAS 1.26:166236
Accession Number
82N25267
Funding Number(s)
CONTRACT_GRANT: NAS2-10464
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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