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Inflatable Space Structures Technology Development for Large Radar AntennasThere has been recent interest in inflatable space-structures technology for possible applications on U.S. Department of Defense (DOD) missions because of the technology's potential for high mechanical-packaging efficiency, variable stowed geometry, and deployment reliability. In recent years, the DOD sponsored Large Radar Antenna (LRA) Program applied this new technology to a baseline concept: a rigidizable/inflatable (RI) perimeter-truss structure supporting a mesh/net parabolic reflector antenna. The program addressed: (a) truss concept development, (b) regidizable materials concepts assessment, (c) mesh/net concept selection and integration, and (d) developed potential mechanical-system performance estimates. Critical and enabling technologies were validated, most notably the orbital radiation durable regidized materials and the high modulus, inflatable-deployable truss members. These results in conjunction with conclusions from previous mechanical-packaging studies by the U.S. Defense Advanced Research Projects Agency (DARPA) Special Program Office (SPO) were the impetus for the initiation of the DARPA/SPO Innovative Space-based Antenna Technology (ISAT) Program. The sponsor's baseline concept consisted of an inflatable-deployable truss structure for support of a large number of rigid, active radar panels. The program's goal was to determine the risk associated with the application of these new RI structures to the latest in radar technologies. The approach used to define the technology maturity level of critical structural elements was to: (a) develop truss concept baseline configurations (s), (b) assess specific inflatable-rigidizable materials technologies, and (c) estimate potential mechanical performance. The results of the structures portion of the program indicated there was high risk without the essential materials technology flight experiments, but only moderate risk if the appropriate on-orbit demonstrations were performed. This paper covers both programs (LRA and ISAT) in two sections, Parts 1 and 2 respectively. Please note that the terms strut, tube, and column are all used interchangeably and refer to the basic strut element of a truss. Also, the paper contains a mix of English and metric dimensional descriptions that reflect prevailing technical discipline conventions and common usage.
Document ID
20040191339
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Freeland, R. E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Helms, Richard G.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Willis, Paul B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Mikulas, M. M.
(Colorado Univ. CO, United States)
Stuckey, Wayne
(Aerospace Corp. United States)
Steckel, Gary
(Aerospace Corp. United States)
Watson, Judith
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
IAC-04-IAF-I.1.10
Meeting Information
Meeting: 55th International Astronautical Congress
Location: Vancouver
Country: Canada
Start Date: October 4, 2004
End Date: October 8, 2004
Funding Number(s)
OTHER: 23R-319-03-9s26-01
Distribution Limits
Public
Copyright
Public Use Permitted.
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