NASA SBIR 2015 Solicitation
FORM B - PROPOSAL SUMMARY
PROPOSAL NUMBER: |
15-2 S1.02-9216 |
PHASE 1 CONTRACT NUMBER: |
NNX15CP76P |
SUBTOPIC TITLE: |
Microwave Technologies for Remote Sensing |
PROPOSAL TITLE: |
ROC-Rib Deployable Ka-Band Antenna for Nanosatellites |
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Tendeg, LLC
686 S Taylor Ave Ste 108
Louisville, CO 80027 - 3000
(303) 929-4466
PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Gregg Freebury
gregg@tendeg.com
686 S Taylor Ave Ste 108
Louisville, CO 80027 - 3000
(303) 929-4466
CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Gregg Freebury
gregg@tendeg.com
686 S. Taylor Ave, Ste 108
Louisville, CO 80027 - 3000
(303) 929-4466
Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 3
End: 6
Technology Available (TAV) Subtopics
Microwave Technologies for Remote Sensing is a Technology Available (TAV) subtopic
that includes NASA Intellectual Property (IP). Do you plan to use
the NASA IP under the award? No
TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
In these days of tight budgets and limited funding, NASA is constantly looking for new ways to reduce development time and costs of future spacecraft. This is the driving spirit behind NASA's increasing interest in the CubeSat platform, and the vision that is guiding development and demonstration of higher-risk technologies that can eventually lead to low-cost atmospheric science from CubeSats. For example, a tantalizing next-generation CubeSat system would combine a high-gain deployable antenna with a high-frequency Ka-band transponder to support very high bandwidth communications on the order of 10s of Mbps and/or very high-resolution radiometric remote sensing of atmospheric phenomenon. To address this need, Tendeg proposes to develop a Ka-band deployable mesh antenna that can package within a 3U CubeSat volume and deploy to diameters of 0.8-1.5m. The antenna employs a backing structure that is a hybrid wrap-rib/perimeter-truss design. A net supports a reflective mesh while the entire assembly provides the structural depth and surface accuracy needed for Ka-band operation.
POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The primary NASA target application for the proposed deployable antenna technology is future NASA CubeSat and SmallSat spacecraft for which communications up/downlink or passive RF remote sensing measurement resolution is a major bottleneck in the system design. In particular, the proposed technology will enable very high bandwidth communications on the order of 10s of Mbps and/or very high-resolution radiometric remote sensing of atmospheric phenomenon.
POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Beyond NASA applications, the proposed deployable antenna technology could see use in other military and commercial applications where data up/downlink or passive RF sensing is also a considerable need. Terrestrial-based applications might include portable military and commercial communication networks that desire Ka-band operations and can benefit from lightweight, man-portable and deployable high-gain apertures.
TECHNOLOGY TAXONOMY MAPPING (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.)
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Actuators & Motors
Analytical Methods
Antennas
Composites
Deployment
Machines/Mechanical Subsystems
Nondestructive Evaluation (NDE; NDT)
Prototyping
Spacecraft Design, Construction, Testing, & Performance (see also Engineering; Testing & Evaluation)
Structures
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Form Generated on 03-10-16 12:21
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