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Practical aspects of instrumentation system installation, volume 13A review of factors influencing installation of aircraft flight test instrumentation is presented. Requirements, including such factors as environment, reliability, maintainability, and system safety are discussed. The assessment of the mission profile is followed by an overview of electrical and mechanical installation factors with emphasis on shock/vibration isolation systems and standardization of the electric wiring installation, two factors often overlooked by instrumentation engineers. A discussion of installation hardware reviews the performance capabilities of wiring, connectors, fuses and circuit breakers, and a guide to proper selections is provided. The discussion of the installation is primarily concerned with the electrical wire routing, shield terminations and grounding. Also inclued are some examples of installation mistakes that could affect system accuracy. System verification procedures and special considerations such as sneak circuits, pyrotechnics, aircraft antenna patterns, and lightning strikes are discussed.
Document ID
19820005267
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Borek, R. W.
(Advisory Group for Aerospace Research and Development Neuilly-Sur-Seine, France)
Pool, A.
(Advisory Group for Aerospace Research and Development Neuilly-Sur-Seine, France)
Sanderson, K. C.
(Advisory Group for Aerospace Research and Development Neuilly-Sur-Seine, France)
Date Acquired
September 4, 2013
Publication Date
September 1, 1981
Publication Information
ISBN: 92-835-1399-1
Subject Category
Aircraft Instrumentation
Report/Patent Number
AGARD-AG-160-VOL-13
NASA-TM-84067
AD-A107355
Accession Number
82N13140
Distribution Limits
Public
Copyright
Other
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