Small Business Innovation Research/Small Business Tech Transfer
Light-weight Self-correcting Inflatable/rigidizable Space Antennas, Phase I
Project Description
The NASA/L'Garde Inflatable Antenna Experiment (IAE)flown in STS-77 has showed the potential of this class of structures in significantly reducing the costs for space access. It also pointed the way to future work. Numerous studies and ground tests on real hardware conducted by L'Garde since then, have shown the extension of these advantages to rigidizable parabolic reflectors and provided further proof for their manufacturability, their significant stowage volume advantages. and their controlled deployment. The most significant issue that remains is their surface accuracy under the influence of, mainly, thermal loads. The structural films laminates that must be used in their construction exhibit positive thermal expansion coefficients adversely affecting their accuracy in the frequency range >1-3 GHz. In Phase 1 of this effort L'Garde and SARA intend to design and analyze a corrective system for inflatable and/or rigidizable antennas comprised of a phased array feed capable of correcting phase errors and a movable feed platform to correct for focal point shifts. If the corrective system feasibility is proven and we proceed to Phase 2, such a system will be designed, built and tested on a subscale inflatable or rigidizable reflector. This system can have profound positive effects on space communications.
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Anticipated Benefits
Potential NASA Commercial Applications: Self-correcting rigidizable appertures can find many terrestrial uses in Terrestrial antennas required in high gain, or high data throughput (as in video) applications, when ease and cost of transporting large apertures is of prime importance, such as during natural or man-made disasters, or a combat theater, where reducing the logistic footprint is of prime importance to armed forces. These types of applications could be much more efficiently accomplished with a rigidizable aperture that inflates to shape in a short time then rigidizes. The rigidization material will be thicker in these applications so that the appertures can sustain themselves with the much more severe loads present in the terrestrial environment (gravity, wind, thermal,e tc.) than those encountered in space.
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Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
Glenn Research Center
(GRC)
|
Lead Organization | NASA Center | Cleveland, Ohio |
| L'Garde, Inc. | Supporting Organization |
Industry
Minority-Owned Business
|
Tustin, California |
Primary U.S. Work Locations
-
California
-
Ohio
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This is a historic project that was completed before the creation of TechPort on October 1, 2012. Available data has been included. This record may contain less data than currently active projects.