|PROPOSAL NUMBER:||06 O1.04-9843|
|SUBTOPIC TITLE:||Antenna Technology for Spacecraft and Planetary Surface Vehicles|
|PROPOSAL TITLE:||Light-weight Self-correcting Inflatable/rigidizable Space Antennas|
SMALL BUSINESS CONCERN
(Firm Name, Mail Address, City/State/Zip, Phone)
15181 Woodlawn Ave.
Tustin, CA 92780-6487
PRINCIPAL INVESTIGATOR/PROJECT MANAGER
(Name, E-mail, Mail Address, City/State/Zip, Phone)
L'Garde, Inc. 15181 Woodlawn Ave.
Tustin, CA 92780-6487
TECHNICAL ABSTRACT ( Limit 2000 characters, approximately 200 words)
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.
POTENTIAL NASA COMMERCIAL APPLICATIONS ( Limit 1500 characters, approximately 150 words)
Light-weight rigidizable antenna appertures that can autonomously correct for surface errors can be widely used in both NASA's Space Science missions and Communications from the outer planets to NASA'S terrestrial facilities and/or earth orbits. Their competitive weight, cost of construction due to their simple manufacturing, and large cost savings due to their very small stowage volume at launch can enable otherwise unaffordable missions, or missions that would be impossible without the use of this class of structures.
POTENTIAL NON-NASA COMMERCIAL APPLICATIONS ( Limit 1500 characters, approximately 150 words)
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.
|NASA's technology taxonomy has been developed by the SBIR-STTR program to disseminate awareness of proposed and awarded R/R&D in the agency. It is a listing of over 100 technologies, sorted into broad categories, of interest to NASA.|
TECHNOLOGY TAXONOMY MAPPING
Architectures and Networks
Autonomous Control and Monitoring
Earth-Supplied Resource Utilization
General Public Outreach
Integrated Robotic Concepts and Systems
Large Antennas and Telescopes
Sensor Webs/Distributed Sensors
Structural Modeling and Tools