DocumentCode
2067477
Title
The design and operation of a lunar dust seal testing system
Author
Anderson, Grant A. ; Iacomini, Christine
Author_Institution
Paragon Space Dev. Corp., Tucson, AZ, USA
fYear
2010
fDate
6-13 March 2010
Firstpage
1
Lastpage
6
Abstract
Depending on your perspective, the need to accommodate shaft seals to mitigate lunar dust hazards is either an interesting mechanical engineering problem or a highly critical technology not yet proven. Due to the unique environment and the inability to test ¿true¿ solutions on Earth, the authors consider the solutions to critical seal design and testing as an `unproven´ technology hurdle that can result in years of delay and significant cost risk. Apollo attempted to mitigate dust effect...and did not succeed. Working with University of Arizona students, Paragon has specified, design and initially tested a ¿lunar dust seals test apparatus¿ that allows for the testing of multiple seals under simulated vacuum conditions using lunar dust simulant. This apparatus is being used to test sealing solution innovations conceived by Paragon engineers. However, it is true that NO testing apparatus on Earth can test seals in a true ¿lunar¿ environment and, ultimately, testing will need to be done.
Keywords
aerospace computing; aerospace instrumentation; cosmic dust; innovation management; planetary atmospheres; seals (stoppers); test equipment; Apollo; Paragon engineers; University of Arizona; cost risk; critical seal design; dust effect; lunar dust hazards; lunar dust seal testing system; lunar dust simulant; lunar environment; mechanical engineering problem; multiple seals; sealing solution innovations; shaft seals; simulated vacuum conditions; testing apparatus; Costs; Delay; Earth; Hazards; Mechanical engineering; Moon; Seals; Shafts; System testing; Technological innovation;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2010 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4244-3887-7
Electronic_ISBN
1095-323X
Type
conf
DOI
10.1109/AERO.2010.5446991
Filename
5446991
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