NASA SBIR 2018-I Solicitation

Proposal Summary


PROPOSAL NUMBER:
 18-1- H10.01-9942
SUBTOPIC TITLE:
 Advanced Propulsion Systems Ground Test Technology
PROPOSAL TITLE:
 Advanced Coating to Mitigate Hydrogen Embrittlement in High Temperature Environments
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Summit Information Solutions, Inc.
4870 Sadler Road, Suite 102
Glen Allen , VA 23060-6294
(804) 201-4399

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Dustin Winslow
dustin.winslow@summitis.com
4870 Sadler Road, Suite 102 Glen Allen, VA 23060 - 6294
(801) 259-5574

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)
Shuganti Caradonna
shuganti.caradonna@summitis.com
4870 Sadler Road, Suite 102 Glen Allen, VA 23060 - 6294
(804) 840-8477
Estimated Technology Readiness Level (TRL) :
Begin: 2
End: 3
Technical Abstract

The failure of metallic parts due to hydrogen embrittlement has been a constant challenge for many industries for decades, and for NASA in particular. The hydrogen embrittlement problems endemic to industries that require heavy use of hydrogen have been solved in various ways. Most of these solutions involve the careful development of alloys that are less susceptible to hydrogen embrittlement. Unfortunately, these alloys often require a sacrifice of some other highly desired material property, such as strength, hardness, ductility, etc. Coatings have also been attempted. However, these coatings and coating techniques have their own drawbacks, which include ceramic coatings that flake off after only a few use cycles and coating techniques that cannot deposit onto a finished part because they require line of sight during deposition. To better mitigate the very pressing hydrogen embrittlement challenge, Summit Information Solutions, Inc. proposes the use of a mature deposition technique that has not seen much use outside of the microelectronics industry. A thin film encapsulate will be deposited onto test samples of Inconel 718 and A-286 austenitic stainless steel. The coating material has a melting temperature in excess of 5500 °C, and is non-reactive with hydrogen. The coated samples’ properties will be tested, and the results will be compared to those of the untreated samples. Summit’s goal for Phase I is to show that the surface treatment is a robust layer at elevated temperatures. The extensive hydrogen embrittlement tests will be conducted in Phase II of the project.

Potential NASA Applications

The success of this feasibility study for a hydrogen embrittlement mitigation layer will have a wide breadth of NASA applications. Several NASA applications that will benefit from the development of this technology include test stand components for engine testing, long term storage of hydrogen in storage vessels, nuclear thermal propulsion applications on the newly developing NTP program, because our proposed surface layer also shows literature evidence of radiation protection, among others.

Potential Non-NASA Applications

Hydrogen embrittlement is a challenge for all industries that require the use of hydrogen around metallic surfaces. The coating we are proposing has seen some initial use in the nuclear industry in reactor vessels. However, traditionally the individual parts must be coated and then joined. This produces seams that are left unprotected after joining. Our deposition technology will allow this already in-use coating technique to be utilized without the drawbacks of piecemeal coating of the parts.


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