NDLI: Low-mass inflation systems for inflatable structures

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Low-mass inflation systems for inflatable structures

Content Provider	NASA Technical Reports Server (NTRS)
Author	Webster, Mark S. Engelbrecht, Carl S. Thunnissen, Daniel P.
Copyright Year	1995
Description	The use of inflatable space structures has often been proposed for aerospace and planetary applications. Communication, power generation, and very-long-baseline interferometry are just three potential applications of inflatable technology. The success of inflatable structures depends on the development of an applications of inflatable technology. This paper describes two design studies performed to develop a low mass inflation system. The first study takes advantage of existing onboard propulsion gases to reduce the overall system mass. The second study assumes that there is no onboard propulsion system. Both studies employ advanced components developed for the Pluto fast flyby spacecraft to further reduce mass. The study examined four different types of systems: hydrazine, nitrogen and water, nitrogen, and xenon. This study shows that all of these systems can be built for a small space structure with masses lower than 0.5 kilograms.
File Size	1073038
Page Count	22
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19960054146
Archival Resource Key	ark:/13960/t9382930s
Language	English
Publisher Date	1995-01-01
Access Restriction	Open
Subject Keyword	Mechanical Engineering Leakage Water Hydrazines Space Erectable Structures Aerospace Environments Xenon Nitrogen Inflatable Space Structures Small Satellite Technology Temperature Effects Self Erecting Devices Orbital Assembly Spacecraft Design Satellite Communication Interferometry Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Article

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