SBIR/STTR Research Award

Silicon Carbide Lightweight Optics With Hybrid Skins for Large Cryo Telescopes

Award identifier ae086d03a75003febae8626ddad2e151c71073ab5d552a6c8d0a3e6a9b657bb7Awarding agency National Aeronautics and Space Administration

Award amount

$99,081

Program and phase

SBIR · Phase I

Award year

2009

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Optical Physics Company
Proposal award date
2009-01-22
Contract end date
2009-10-22
UEI
NNMCZN2CS7D9
Solicitation number
Not reported
Topic code
S2.04

Research abstract

Optical Physics Company (OPC) proposes to manufacture new silicon carbide (SiC) foam-based optics that are composite, athermal and lightweight (FOCAL) that provide an enabling capability for performing NASA space missions that will require 2 to 3 meter class cryogenic mirrors for large infrared telescopes. Open-cell foam core mirror technology has evolved over the past ten years and has produced somewhat large (0.5 m dia.), lightweight (<10 kg/m2), rapidly and uniformly cryo-cooled and dimensionally stable (tested to 25 K) mirrors configured with monolithic chemical vapor deposited (CVD) skins. Significant problems have arisen as the size has increased that prevent their use on large aperture telescopes. These problems include the inherent stress in the monolithic skins which can result in skin cracking during the substrate manufacturing and finishing processes, the non-uniformity of the .040"-.050" thick monolithic skins that typically require .010"-.015" of material removal before a continuous surface can be achieved for optical finishing, the long schedule of manufacturing the mirror substrate, and the large $2M/m2 cost to produce the polished mirror. OPC proposes an innovation where the monolithic SiC skins are replaced with SiC fiber reinforced/SiC CVD skins. This hybrid design consists of a .020"-.030" thick SiC fiber reinforced layer ground to a smooth finish and near net shape, and then post coated with a .005"-.010" thick CVD SiC polishing layer. This provides increased skin strength and toughness to enable the technology to produce meter class mirrors without skin cracking. The manufacturing time and CVD chamber cost are reduced because premanufactured SiC fibers are used to provide the bulk of the skin mass rather than laying down a monolithic skin atom by atom via CVD. The net effect is to produce a SiC FOCAL mirror substrate that is stronger, tougher, scalable to meter class, and potentially better than 50% faster and cheaper to manufacture.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

70 SBIR/STTR records share this UEI (2001–2021). Reported award amounts total $35,389,096. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Commerce, Department of Energy

Agency intelligence

National Aeronautics and Space Administration

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