NASA SBIR 2018-I Solicitation

Proposal Summary


PROPOSAL NUMBER:
 18-1- Z10.03-6443
SUBTOPIC TITLE:
 Nuclear Thermal Propulsion (NTP)
PROPOSAL TITLE:
 More Ductile Bulk Tungsten
SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Transition45 Technologies, Inc.
1739 North Case Street
Orange , CA 92865-4211
(714) 283-2118

Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)
Edward Chen
transition45@sbcglobal.net
1739 North Case Street Orange, CA 92865 - 4211
(714) 283-2118

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)
Edward Chen
transition45@yahoo.com
1739 North Case Street Orange, CA 92865 - 4211
(714) 283-2118
Estimated Technology Readiness Level (TRL) :
Begin: 2
End: 4
Technical Abstract

This SBIR Phase I effort will develop and demonstrate a novel manufacturing process based on severe plastic deformation (SPD) to refine and enhance the microstructure-properties of bulk tungsten. Tungsten, with its many unique characteristics, plays an important role in nuclear reactors including for the nuclear thermal propulsion engine. The refractory metal, however, still has a number of shortcomings which still need to be addressed. These include a high ductile-to-brittle transition temperature, low ductility and poor fracture toughness, low machinability and fabricability, low-temperature brittleness, radiation-induced brittleness, and a relatively low recrystallization (RX) temperature compared to its operation temperature. The use of W above its RX temperature interminably can be unsafe because its mechanical properties decrease in such an environment. Low-temperature brittleness also imposes restrictions on the application of W as a structural material. And, given its high hardness, high brittleness, and poor machinability, W parts can be very costly and time-consuming to manufacture. Past efforts to increase the ductility of W were primarily directed on alloying, grain refinement, extreme working, area reductions, impurity reductions, and heat treatments. While ductile W currently exists in wire form (e.g., filaments) through extensive working and area reduction, this approach is clearly not practical for applications where bulk size parts are needed.

Potential NASA Applications

High temperature shielding structures and hot gas path nozzles and thrusters for diverse spacecraft and rocket propulsion systems including the nuclear thermal propulsion engines will benefit from a more ductile bulk tungsten material. Other applications include hot structures and heat shields for reusable launch vehicles and/or aircraft engines.

Potential Non-NASA Applications

High temperature shielding structures and hot gas path nozzles and thrusters for diverse commercial and military spacecraft and rocket propulsion systems will benefit from this material. Other applications includes structures and components for reusable launch vehicles, nuclear reactors, gas turbines (both aircraft and industrial), armaments and munitions, and chemical process equipment. Even more applications will open up if tungsten's low ductility can be improved.


Form Generated on 05/25/2018 12:03:27