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ISOBUS: A new versatile spacecraft platform using Shuttle small payloadsThe new NASA credo of 'faster, better, cheaper' calls for a new generation of smaller and less complex spacecraft. In response to this challenge, many new spacecraft concepts have been generated within NASA, industry, and academia. The JPL, Rockwell International Space Systems Division, and The Space Dynamics Laboratory (SDL)/Utah State University (USU) are jointly examining one such new spacecraft concept, hereafter termed ISOBUS, which is derived from recent research and development work in isogrid structures based on a six-sided hexagon shaped structure. Two prototypical products from SDL/USU's work are ISOSPACEPACK and ISOSAT. These hexagon shaped elements serve as building blocks for the ISOBUS spacecraft concept. Various aspects of the ISOBUS concept are discussed.
Document ID
19940014710
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tamir, David
(Rockwell International Corp. Cocoa Beach, FL, United States)
Ridenoure, Rex W.
(Jet Propulsion Lab. California Inst. of Tech., Pasadena., United States)
Moore, R. Gilbert
(Utah State Univ. Logan., United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1993
Publication Information
Publication: NASA. Goddard Space Flight Center, The 1993 Shuttle Small Payloads Symposium
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
94N19183
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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