NDLI: Space-frame lunar lander

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Space-frame lunar lander

Content Provider	NASA Technical Reports Server (NTRS)
Author	Curtis, Steven A.
Copyright Year	2010
Description	The space-frame lunar lander was originally intended to (1) land on rough lunar terrain, (2) deform itself to conform to the terrain so as to be able to remain there in a stable position and orientation, and (3) if required, further deform itself to perform various functions. In principle, the space-frame lunar lander could be used in the same way on Earth, as might be required, for example, to place meteorological sensors or a radio-communication relay station on an otherwise inaccessible mountain peak. the space-frame lunar lander would include a truss-like structure consisting mostly of a tetrahedral mesh of nodes connected by variable-length struts, the lengths of which would be altered in coordination to impart the desired overall size and shape to the structure. Thrusters (that is, small rocket engines), propellant tanks, a control system, and instrumentation would be mounted in and on the structure (see figure). Once it had landed and deformed itself to the terrain through coordinated variations in the lengths of the struts, the structure could be further deformed into another space-frame structure
File Size	260122
Page Count	2
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_20100001347
Archival Resource Key	ark:/13960/t1bk6bw8z
Language	English
Publisher Date	2010-01-01
Access Restriction	Open
Subject Keyword	Spacecraft Design, Testing And Performance Microelectromechanical Systems Deformation Lunar Topography Tetrahedrons Lunar Landing Modules Struts Lunar Landing Sites Shapes Trusses Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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