SBIR/STTR Research Award

Resin Additive Manufacturing Processed Thermal Protection Systems (RAMP TPS)

Award identifier 2e4013737c4566a2809f485cd465ff635a53ee0f701535b180b611525acd8361Awarding agency National Aeronautics and Space Administration

Award amount

$124,900

Program and phase

STTR · Phase I

Award year

2019

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
TETHERS UNLIMITED, INC.
Proposal award date
2019-08-19
Contract end date
2020-09-18
UEI
FHC2EKAPYU47
Solicitation number
STTR_19_P1
Topic code
T12

Research abstract

Tethers Unlimited, Inc. (TUI) and Western Washington University (WWU) propose to develop the ldquo;Resin Additive Manufacturing Processed Thermal Protection Systemrdquo; (RAMP TPS), an in-situ cured, additively manufactured, spacecraft heat shield material and process.nbsp;nbsp;RAMP TPS uses Direct Ink Writing (DIW) of an optimized benzoxazine resin-based compound, filled with carbon fibers, silica micro-balloons, cure accelerators, and viscosity modifiers.nbsp;nbsp;Current TPS systems are expensive to produce, and they make various compromises in their heat shield performance properties.nbsp;nbsp;The RAMP TPS effort will leverage automation techniques borrowed from 3D printing, along with state of the art heat shield materials, while adding the ability to cure in-situ during robotic deposition.nbsp;nbsp;RAMP TPS will offer superior mass-effectiveness through optimized material composition as well as graded low density printed core structures.nbsp;nbsp;While conventional TPS resins can require hours for an oven cure process, WWUrsquo;s Benzoxazine formulation will use accelerator additives to chemically set within minutes of deposition using the heat supplied by TUIrsquo;s feedhead assembly.nbsp;Initial heat shield performance characterization will be performed using density, strain at break, thermal conductivity, TGA measurements, and thermo-oxidative ablation testing with an oxy-acetylene torch.nbsp;nbsp;This novelnbsp;nbsp;heat shield technology will have near term applications in lowering the cost of high-performance spacecraft production, as well as future applications within TUIrsquo;s in-space processes for automated production and servicing of re-entry vehicles.nbsp;nbsp;

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

86 SBIR/STTR records share this UEI (1992–2019). Reported award amounts total $32,140,882. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: National Aeronautics and Space Administration, Department of Defense

Agency intelligence

National Aeronautics and Space Administration

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