SBIR/STTR Research Award

A Modular In-Situ Curing Apparatus for Thermoset Resin Mixtures Applied as Thermal Protection Systems

Award identifier dd1b11115a1ef2c4953ae0a114b9b51dbe6a4f4f001103e78f9835eab283b2d0Awarding agency National Aeronautics and Space Administration

Award amount

$754,921

Program and phase

STTR · Phase II

Award year

2021

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
INTELLIGENT OPTICAL SYSTEMS, INC.
Proposal award date
2021-08-20
Contract end date
2023-08-19
UEI
NLDHG92SMX37
Solicitation number
STTR_19_P2
Topic code
T12

Research abstract

Future human extraterrestrial missions will require export and landing of countless payloads on the lunar and Martian surfaces. Such a quantity and rate of payload delivery will require cost-effective and rapid manufacturing of many large Thermal Protection Systems (TPS). Intelligent Optical Systems proposes to develop a modular system for in-situ bonding and curing of thermoset resin to the spacecraft to facilitate automated manufacturing of TPS. This system is compatible with additive manufacturing techniques, high-temperature thermoset resins, and composite substrates currently in use and under development by NASA, SpaceX, and others. Our in-situ resin curing system will eliminate the need for large ovens or autoclaves. By leveraging advances in out of autoclave curing methods, our system will enable curing of additively manufactured high temperature thermoset resin based TPS in-situ. An infrared heat source mounted directly on the print head will rapidly stiffen the extrudate as it leaves the nozzle, enabling multi-layer printing. Upon completion of the printing process, a modular system of conductive heat blankets, conforming to the surface contours of the structure, will control final cure of the thermoset. The system will measure the temperature of the resin, and provide feedback control and log thermal history during curing. In-line surface activation with a corona generator will ensure strong bonding to the underlying substrate and at layer interfaces.Validation of the system will be performed by measuring the degree of cure of in-situ cured samples and measurement of bond strength. We have already demonstrated in Phase I that in-situ cured samples achieve a high degree of cure, char yield, glass transition temperature, and bond strength, comparable to traditionally cured resins. The target end point for Phase II work is scaling the system by 10x with performance deviation of no more than 5% between in-situ cured and control cured resins.

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

264 SBIR/STTR records share this UEI (1998–2025). Reported award amounts total $77,140,779. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, Department of Health and Human Services, National Aeronautics and Space Administration, Department of Energy, Environmental Protection Agency, Department of Agriculture

Agency intelligence

National Aeronautics and Space Administration

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