NASA SBIR 2016 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 16-1 S2.03-8014
SUBTOPIC TITLE: Advanced Optical Systems and Fabrication/Testing/Control Technologies for EUV/Optical and IR Telescope
PROPOSAL TITLE: Ultra-Stable Zero-CTE HoneySiC and H2CMN Mirror Support Structures

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Fantom Materials, Inc.
3038 Aukele Street
Lihue, HI 96766 - 1464
(808) 245-6465

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr William Fischer III
bill.fischer@fantommaterials.com
3038 Aukele Street
Lihue, HI 96766 - 1464
(570) 899-4191

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr William Fischer III
bill.fischer@fantommaterials.com
3038 Aukele Street
Lihue, HI 96766 - 1464
(570) 899-4191

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 5
End: 6

Technology Available (TAV) Subtopics
Advanced Optical Systems and Fabrication/Testing/Control Technologies for EUV/Optical and IR Telescope 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)
NASA MSFC, GSFC and JPL are interested in Ultra-Stable Mirror Support Structures for Exoplanet Missions. Telescopes with Apertures of 4-meters or larger and using an internal coronagraph require a telescope wavefront stability that is on the order of 10 pico-meters RMS per 10 minutes. Interest is also for IR/FIR missions requiring 8-meter or larger diameter mirrors with cryogenic deformations <100 nm RMS. Fantom Materials is specifically responding to the need for ultra-stable mirror support structure traceable to the needs of Cosmic Origins for UVOIR, Exo and FIR telescopes, including mirror support structures, whiffle plates, delta frames and strongbacks. HoneySiC material has multiple features that make it very attractive as a potential future deployment hinge and latching material: 1) It's an additively manufactured Ceramic Matrix Composite (CMC) with no Coefficient of Moisture Expansion (CME). Individually molded parts become a monolithic construct, thus it is possible to manufacture an entire telescope using HoneySiC, 2) It's extremely light weight; laminate HoneySiC sheets have the same density as beryllium and honeySiC panels have about 1/5 the density of beryllium, 3) It's extremely dimensionally stable due to a zero-CTE across a temperature range of -200 to +25C. The thermal conductivity can be supercharged by addition of extremely high thermal conductivity carbon nanotubes. To achieve a stability of 10 picometer (e.g., LISA gravity wave detector mission) will require the distortion parameters to go to zero for a passive material. The overarching objectives of the project are to collaborate with NASA MSFC, GSFC, JPL and Northrop Grumman to demonstrate new mirror mounting materials with ultra-stability. Potentially every beryllium and M55J-954-6 part could be replaced by HoneySiC, resulting in a massive reduction in labor and schedule, as well as weight. Stiffness and dimensional stability would be greatly enhanced by HoneySiC or H2CMN.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
From the present state-of-the-art it will take an 8 order-of-magnitude improvement in materials stability This project is the point of departure for ultra-stable mirror support structures made using first-generation zero CTE HoneySiC (circa 2014), and 2nd generation Hierarchical Hybrid Ceramic Matrix Nano-composite (H2CMN, circa 2016). These extremely promising engineered ceramic matrix composite materials will replace the status quo, moisture-absorbing, organic matrix composites used in the present state-of-the-art composites, as well as to directly replace beryllium. 1st and 2nd generation HoneySiC will provide the low areal cost, low areal density, low cost and ultra-stability that is required for future EUV, UV/O and Far-IR mission telescopes.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Low cost, lightweight, dimensionally stable HoneySiC material has use in complex telescopes for Astronomy, Imaging and Remote Sensing applications, including optical instruments/telescopes which enable imaging, surveillance, and reconnaissance missions for police and paramilitary units, fire fighters, power and pipeline monitoring, search and rescue, atmospheric and ocean monitoring, imagery and mapping for resource management, and disaster relief and communications. The dual-use nature of complex telescopes will bring affordability to national defense missions as well.

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
Composites
Distribution/Management
Optical
Polymers
Telescope Arrays
Ultraviolet
Visible

Form Generated on 04-26-16 15:14