SBIR/STTR Research Award

Multifunctional Thermal Protection System for Future Space Transportation Vehicles

Award identifier 8d8311e1ed1931331c4965d91f01341dc343552c8de163ff032c9e84a4b2b306Awarding agency National Aeronautics and Space Administration

Award amount

$99,972

Program and phase

SBIR · Phase I

Award year

2002

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
ULTRAMET
Proposal award date
Not reported
Contract end date
Not reported
UEI
N8ZRMWX85NZ6
Solicitation number
Not reported
Topic code
Not reported

Research abstract

Current and developmental thermal protection system (TPS) materials severely limit the flight path and thus the mission flexibility of existing and future space transportation vehicles (STV), including reusable launch vehicles (RLV). TPS are essential, but also add parasitic weight rather than providing both structural functionality and thermal protection. Multifunctional TPS with structural capability would be highly desirable. TPS are also subject to severely limited life due to rapid failure or need for replacement if the outer surface or coating suffers damage. As a result, self-healing TPS would be substantially beneficial or could even be essential if self-repair is needed for mission survivability. Multifunctional and self-healing TPS must also be fabricable as large-scale and cost-effective panels if they are to be more widely used for acreage type applications. The objective of the proposed project is to overcome the known limitations of current insulating materials (e.g. AETB, FRCI, SIRCA) and to further enhance capabilities over TPS that are currently under development by demonstrating the feasibility of an innovative, multifunctional and self-healing TPS suited for varied STV and related applications. The unique TPS proposed in this project will provide an unequaled combination of structural and thermal performance, large cross-section fabricability and low fabrication cost. The proposed approach builds on developments already initiated and demonstrated in complementary efforts but adds multiple innovative features. Specifically, the new TPS will combine a carbon aerogel-filled, carbon foam core structure with an innovative, lower cost and larger scale aerogel infiltration method and self-healing carbon/carbon facesheets to produce a highly enhanced and more cost-effective TPS. Previous work has shown that the carbon aerogel-filled, carbon foam core structure provides low thermal conductivity and high temperature capability.

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.

Research funding history

380 SBIR/STTR records share this UEI (1983–2025). Reported award amounts total $105,154,309. Reported amounts are not federal obligations.

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

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy, National Science Foundation, Department of Transportation, Department of Health and Human Services

Agency intelligence

National Aeronautics and Space Administration

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