SBIR/STTR Research Award

Feature-aware Ablation and Reaction Simulator for Thermal Extremes

Award identifier 7db041a92a990a4430e45525cbb19fc7d784873891dd6024299bc4c79d75c658Awarding agency Department of Defense · Navy

Award amount

$999,999

Program and phase

STTR · Phase II

Award year

2025

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Award details

Awarding agency
Department of Defense
Branch
Navy
Recipient company
SPECTRAL SCIENCES, INC
Proposal award date
2025-05-08
Contract end date
2027-05-12
UEI
N8CQNLSSAZY4
Solicitation number
23.A
Topic code
N23A-T026

Research abstract

Hypersonic vehicles require thermal protection systems (TPS) for protection from high-temperature, strongly shocked air. Carbon-based ablative TPS have received particular attention for Navy applications. Since ground-based testing at flight-like non-equilibrium conditions is limited and costly, physics-based simulation tools, including comprehensive finite-rate gas-gas and gas-surface chemistry models, are essential for designing next-generation TPS materials. The intricate interplay between gases and materials during hypersonic flight induces a degradation process, leading to alterations in surface morphology, and subsequently influencing the ablation dynamics within the TPS material. Moreover, these morphological/surface transformations have the potential to impact the gas-surface interactions throughout the flight. However, the current finite-rate ablation models for these systems are not tuned to chemical and morphological structure of the TPS material and do not account for mesoscale structural changes that occur during a flight. To address these gaps, Spectral Sciences, Inc. (SSI), in collaboration with the University of Colorado Boulder (CU), the University of Minnesota (UMN) and GoHypersonic, Inc. (GHI), proposes to develop an innovative software suite to model ablation of carbon-based TPS materials on hypersonic vehicles, with finite-rate chemistry and mesoscale material physics in the framework of computational fluid dynamics (CFD). Our team combines expertise in both hypersonic vehicle simulations and state-of-the-art experimental gas-surface reaction dynamics. In the Phase I effort, we demonstrated the feasibility of extensions to the state-of-the-art Air Carbon Ablation (ACA) finite-rate model, informed by new experimental data and integrated into the US3D hypersonic CFD code. In the Phase II program, we will implement advanced models of molecular and mesoscale ablation processes, guided by a comprehensive experimental validation campaign on Navy-relevant materials. The final product will meet critical Government and commercial needs to understand and manage gas–material interactions in extreme thermal environments.

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

349 SBIR/STTR records share this UEI (1983–2026). Reported award amounts total $142,164,659. Reported amounts are not federal obligations.

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

Agencies: Department of Defense, Department of Energy, National Aeronautics and Space Administration, National Science Foundation, Department of Agriculture, Department of Homeland Security

Agency intelligence

Department of Defense

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