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Award details
- Awarding agency
- National Aeronautics and Space Administration
- Branch
- Not reported
- Recipient company
- CFD Research Corporation
- Proposal award date
- 2020-09-09
- Contract end date
- 2022-09-08
- UEI
- V3KCP1HNFM33
- Solicitation number
- SBIR_19_P2
- Topic code
- Z7
Research abstract
The regolith particle flow induced by propulsive spacecraft landing on the unprepared surfaces of Moon and Mars occurs in a combination of complex environments that combine low gravity, little or no atmosphere, with rocket exhaust gas flow that is supersonic and partially rarefied, and unusual mechanical properties of the regolith. Of these environmental factors, characterizing the regolith granular material fluidic behavior and gas-granular interactions is the most complex and least developed. In modeling these flows, constitutive relationships are incorporated as collisional, kinetic and frictional stresses as well as drag terms due to momentum exchange with the carrier phase, which become increasingly complex with increasing particle cloud density, compressibility effects in supersonic gas flow, and complexity of multi-size irregularly shaped particle mixtures. Formulation and validation of these closure models is very difficult, mainly due to lack of experimental data covering the broad range of operating conditions and variables. This project aims to generate first of their kind experimental data for gas-granular interaction physics in relevant conditions and implement a constitutive model formulation, maturation and implementation process to arrive at accurate predictive modeling tools for NASA lander project support. In the Phase I, an integrated approach for developing a combined measurement and modeling methodology to further improve accuracy of the gas granular flow solvers used for analysis and design was developed and demonstrated. Targeted experiments analyzing gas-particle flows in high-speed dilute conditions were conducted. Model improvements were made and further modeling requirements were identified.nbsp; In Phase II the parametric space for gas-particle flows, and conditions will be expanded.nbsp; Model improvements to gas-granular flow solver will be based on information obtained from high-resolution simulations and experimental data.nbsp;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.
Research funding history
947 SBIR/STTR records share this UEI (1987–2026). Reported award amounts total $350,893,199. 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 Health and Human Services, National Science Foundation, Department of Commerce, Department of Energy
Agency intelligence
National Aeronautics and Space Administration
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