DocumentCode
1333607
Title
The unique airplane environment effect on electronic equipment
Author
Geiser, David T.
Author_Institution
Boeing Airplane Company, Wichita Div.
fYear
1952
fDate
4/1/1952 12:00:00 AM
Firstpage
14
Lastpage
19
Abstract
Reviewing known factors, this discussion shows airplane environment unique only in the magnitude and rate of change of environment transitions. This effect increases with aircraft performance, intensifying undesirable environment effects. Some basic design approaches are given to minimize both transition and steady-state airframe environment effects, and the environment transition is presented as a useful design tool.
Keywords
Aerospace electronics; Airplanes; Humidity; Insulation; Ionization; Moisture; Sea level;
fLanguage
English
Journal_Title
Airborne Electronics, Transactions of the IRE Professional Group on
Publisher
ieee
ISSN
2168-0213
Type
jour
DOI
10.1109/TPGAE.1952.6594718
Filename
6594718
Link To Document