NASA SBIR 2018-I Solicitation

Proposal Summary


PROPOSAL NUMBER:
 18-1- S2.03-7013
SUBTOPIC TITLE:
 Advanced Optical Systems and Fabrication/Testing/Control Technologies for EUV/Optical and IR Telescope
PROPOSAL TITLE:
 Ultra-Stable ALLVAR Alloy Development for Space Telescopes
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Thermal Expansion Solutions, Inc.
501 Graham Road
College Station , TX 77845-9662
(956) 789-3723

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. James Monroe
jamesamonroe@allvaralloys.com
501 Graham Road College Station, TX 77845 - 9662
(956) 789-3723

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. James Monroe
jamesamonroe@allvaralloys.com
501 Graham Road College Station, TX 77845 - 9662
(956) 789-3723
Estimated Technology Readiness Level (TRL) :
Begin: 2
End: 3
Technical Abstract

This NASA SBIR Phase I proposal is in response to the need for Ultra-Stable Telescope Structures and is designed to evaluate ALLVAR Alloys for their potential as metering and support structures for optics that are critical to NASA’s future missions. Telescopes used for astrophysics, exoplanet, and planetary studies require picometer stability over several minutes to hours. Building large support structures with picometer level stability is a challenge with currently available materials due to their brittle nature in the case of Zerodur and ULE or their requirement to have tight thermal control in the case of SiC or carbon fiber composites. ALLVAR Alloys offer a new material solution for thermally stable structures. They exhibit negative thermal expansion and can compensate for the positive thermal expansion of other materials to stabilize a telescope. The ultimate goal of this work is to create an ultra-stable ALLVAR Alloy metering structure manufacturing process. Bars with low thermal expansion have previously been made by welding ALLVAR Alloys to commercially available Titanium alloys, but their dimensional stability over thermal fluctuations is above the pm stability limit. This Phase I project is designed to better understand the individual stability of the titanium and ALLVAR Alloys and to evaluate hydroxide bonding for mounting mirrors to ALLVAR in preparation for pm level stability tests. The Phase II project would run full scale pm level stability tests in an effort to evaluate the relaxation manufacturing steps and understand how welding the ALLVAR Alloy to titanium may affect the material’s stability.

Potential NASA Applications

A new material with picometer stability can potentially improve support structures for optic systems critical to NASA’s Science Mission Directorate, like LUVIOR or HabEX. There are other potential opportunities in the manufacture of ultra-stable coronograph hardware, support structures for deformable mirrors, telescope steering, and star tracker markets. ALLVAR metals can also be used to make balloon telescopes for exoplanet discovery and cryogenic far infrared telescopes.

Potential Non-NASA Applications

ALLVAR’s unique negative thermal expansion properties can compensate for thermal focus shift in refractive infrared optics used for nightvision, UVAs, missiles, and sub-sea applications. This allow infrared optics manufacturers to reduce the size and weight of their optics. ALLVAR Alloy’s unique properties are also starting to get the attention of composite and glass companies. We see potential collaboration with companies in these areas for support hardware and transition piece applications.


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