NASA SBIR 2010 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 10-1 S2.04-9269
SUBTOPIC TITLE: Advanced Optical Component Systems
PROPOSAL TITLE: Silicon Carbide Corrugated Mirrors for Space Telescopes

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Trex Enterprises Corporation
10455 Pacific Center Court
San Diego, CA 92121 - 4339
(858) 997-9508

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Clifford T. Tanaka
ctanaka@trexhawaii.com
3038 Aukele St.
Lihue, HI 96766 - 1464
(808) 245-6465

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 3
End: 4

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
Trex Enterprises Corporation (Trex) proposes technology development to manufacture monolithic, lightweight silicon carbide corrugated mirrors (SCCM) suitable for NASA space telescopes. The manufacturing process for SCCM integrates Trex's patented CVC SiC process technology with ITT's corrugated mirror design. The former technology CVC SiC has been shown to yield an excellent, highly mechanically and thermally stable mirror substrate material, while the latter corrugated mirror concept has been utilized to rapidly and inexpensively fabricate glass mirrors. The SCCM process forms a hollow, closed back corrugated mirror blank by sequentially depositing thin (1-3mm thick) CVC SiC layers onto appropriately designed sacrificial graphite mandrels, which are removed subsequently by burnout in an oxidizing high temperature furnace. Nominally, the hollow SCCM then consists of mirror facesheet layer, a corrugated interior layer and a backsheet layer, each intimately chemically bonded with each other by the CVC SiC layer-on-layer deposition process. The result is a monolithic, highly stiff, mechanically and thermally stable mirror substrate suitable for visible, UV, EUV, x-ray and infrared telescopes. Furthermore, because of the unique fabrication process, minimal after deposition grinding is required, resulting in a cost-effective, rapid deposition process.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Potential NASA applications include UV/optical telescopes such as ATLAST and IR telescopes such as SAFIR/CALISTO, which would benefit from reduced cost of meter-class SiC mirror blanks. The monolithic SCCM substrate will be polishable to visible/UV quality, with surface figure better than 25nm RMS and surface roughness less than 10 Å RMS. Furthermore, cryogenic IR missions will benefit from CVC SiC highly uniform and near zero CTE at cryogenic temperatures, which is expected to outperform any composite, two-phase material solution.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Lightweight SCCM substrates would have utility in space and airborne telescopes, especially defense-oriented applications (surveillance, tracking, directed energy, etc.). Ground based astronomical observatories utilizing a large aperture segmented primary mirror could also employ SCCM. There may also be utility for the technology in commercial optics for lithography.

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.)
Ceramics
Mirrors
Processing Methods


Form Generated on 09-03-10 12:12