SBIR/STTR Research Award

More Ductile Bulk Tungsten

Award identifier 2c9b99a053fa4f4a27f8448d070bb6aa57711aa23f1a46b36a3c70b2baac023dAwarding agency National Aeronautics and Space Administration

Award amount

$750,000

Program and phase

SBIR · Phase II

Award year

2019

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
TRANSITION45 TECHNOLOGIES INC
Proposal award date
2019-08-13
Contract end date
2021-08-12
UEI
MA7MZBUBZP75
Solicitation number
SBIR_18_P2
Topic code
Z10

Research abstract

This SBIR Phase II effort will continue to develop and then scale up a novel manufacturing process based on severe plastic deformation (SPD) to refine and enhance the microstructure-properties of bulk tungsten.nbsp; Tungsten, with its many unique characteristics, plays an important role in nuclear reactors including for the nuclear thermal propulsion (NTP) engine.nbsp; The refractory metal, however, still has a number of shortcomings which still need to be addressed.nbsp; These include a high ductile-to-brittle transition temperature (DBTT), 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.nbsp; The use of W above its RX temperature interminably can be unsafe because its mechanical properties decrease in such an environment.nbsp; Low-temperature brittleness also imposes restrictions on the application of W as a structural material.nbsp; And, given its high hardness, high brittleness, and poor machinability, W parts can be very costly and time-consuming to manufacture.nbsp; Past efforts to increase the ductility of W were primarily directed on alloying, grain refinement, extreme working, area reductions, impurity reductions, and heat treatments.nbsp; 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.nbsp; Thus, a compaction deformation method under both controlled pressure and temperature along with compressive and shear deformation in a hot die system will be demonstrated here to quot;ductilizequot; W.

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

30 SBIR/STTR records share this UEI (2006–2022). Reported award amounts total $7,496,216. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

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

Agency intelligence

National Aeronautics and Space Administration

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