Electron Kinetics in Hypersonic Plasmas

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$124,954.00
Award Year:
2012
Program:
SBIR
Phase:
Phase I
Contract:
NNX12CF24P
Award Id:
n/a
Agency Tracking Number:
114122
Solicitation Year:
2011
Solicitation Topic Code:
A2.06
Solicitation Number:
n/a
Small Business Information
AL, Huntsville, AL, 35805-1944
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
Y
Duns:
185169620
Principal Investigator:
Vladimir Kolobov
Principal Investigator
(256) 726-4847
proposals-contracts@cfdrc.com
Business Contact:
Silvia Harvey
Business Official
(256) 726-4858
sxh@cfdrc.com
Research Institution:
Stub




Abstract
The goal of this SBIR project is to advance the state-of-the-art in computations of hypersonic plasmas by adding high-fidelity kinetic models for electrons. Electron kinetics affects plasma-chemical reactions and nonequilibrium radiation, which are important for designing hypersonic vehicles. We will develop adaptive multi-scale models for electrons applicable for hypersonic flows in rarefied and continuum regimes using a hierarchy of kinetic and fluid solvers. During Phase 1, a framework for simulation electron kinetics will be added to our existing Unified Flow Solver. Initial testing will be performed to illustrate the feasibility of adaptive multi-scale simulations of electrons using three options: a) fluid model for high plasma densities, b) local Fokker-Planck solver for the Electron Energy Distribution Function, and c) spatially inhomogeneous (nonlocal) Fokker-Planck solver for rarefied flow regimes. In Phase 2, we plan to fully develop and validate the new models versus laboratory experiments. Increased predictive capabilities will be illustrated for the shock layer radiation in the poorly understood vacuum ultraviolet part of the spectrum. We will demonstrate the new tool for hypersonic vehicles with realistic 3D geometries. The effects of electric fields generated by the plasma and externally applied electric and magnetic fields will be taken into account to study discharges and MHD interactions. We will simulate the extreme entry environment at Earth and Mars entry.

* information listed above is at the time of submission.

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