SBIR/STTR Research Award

Concurrent High-Fidelity Measurements and Simulations for Advancing the Design of Rotating Detonation Engines

Award identifier b58f419d1f3c341ebf1d4416c4ce0cdc9144f7c2f1abfefaf22ebbfa806d9dd0Awarding agency National Aeronautics and Space Administration

Award amount

$749,803

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
SPECTRAL ENERGIES LLC
Proposal award date
2021-01-19
Contract end date
2023-01-18
UEI
C3DAVH4VJDG3
Solicitation number
STTR_19_P2
Topic code
T2

Research abstract

The rocket rotating detonation engine (RDE) is a promising technology for its potential large improvement over state-of-the-art alternatives. NASA has identified the RDE as a technology of interest for its in-space propulsion applications such as orbital transfer or planetary lander engines. However, a technology feasibility assessment is not currently possible since the dynamics of the key fluid-combustion-system processes are not well understood for relevant conditions. To achieve a reliable and efficient RDE, various processes must be understood and/or optimized including the fuel-oxidizer propellant mixing, injection of fresh propellants with minimal pressure losses, and the interaction of fresh propellants with combustion products while avoiding deflagration losses. For liquid RDE combustion, measurements simply do not exist that provide detailed characterization of liquid breakup, atomization, vaporization, and burning during the interaction of liquid propellants with shocks and detonation waves.nbsp;The proposed research focuses on transitioning state-of-the-art, time-resolved measurement techniques to liquid-fueled RDEs to provide information critical for understanding these systems and their design. The proposed research will provide ultra-high-speed (100 kHzndash;5 MHz) in-situ spatially and temporally resolved imaging of the gaseous oxidizer-liquid fuel mixing, species concentrations, and combustion to anchor and improve numerical modeling predictive capability.nbsp;The proposed imaging measurements will characterize and measure the gaseous oxygen-liquid fuel mixing, combustion processes, flowfield structure, and dynamics in the liquid-fueled RDEs.nbsp;Concurrent simulations will be performed at two fidelity levels (a lower fidelity Unsteady Reynolds Averaged Navier Stokes model and a higher fidelity shock-physics/multiphase-combustion mode), enabling improved interpretation of the measurement data and RDE physics, and anchored modeling and simulations.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.

Research funding history

272 SBIR/STTR records share this UEI (2007–2026). Reported award amounts total $120,780,215. 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, Department of Health and Human Services, Department of Agriculture

Agency intelligence

National Aeronautics and Space Administration

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