Advanced Reentry Vehicle and Wake Models

Award Information
Agency:
Department of Defense
Branch
n/a
Amount:
$100,000.00
Award Year:
2011
Program:
SBIR
Phase:
Phase I
Contract:
HQ0147-11-C-7542
Award Id:
n/a
Agency Tracking Number:
B103-023-0353
Solicitation Year:
2010
Solicitation Topic Code:
MDA10-023
Solicitation Number:
2010.3
Small Business Information
714 E. Monument Ave, Suite 201, Dayton, OH, -
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
780026220
Principal Investigator:
Travis Drayna
Sr. Engineer
(651) 784-3662
travis.drayna@gohypersonic.com
Business Contact:
Lance Jacobsen
President
(937) 531-6678
lance.jacobsen@gohypersonic.com
Research Institute:
Stub




Abstract
At hypersonic flow conditions, the flow field around reentry vehicles is ionized, resulting in electro-optical emissions, detectable radar cross-sections, and attenuation of signals transmitted through the plasma. Ablative heat shields may further increase the levels of electrons in the plasma around the hardbody and in the wake. We propose to extend an existing high-fidelity computational fluid dynamics code to provide accurate flow field simulation data and to couple with existing signature prediction tools. This code, US3D, is a highly scalable implicit unstructured grid method designed for hypersonic flow simulations. It has been used successfully on a wide variety of reentry vehicles, and has a general thermo-chemical nonequilibrium kinetics model that is extensible to the modeling of complex reentry plasma flow fields. Key elements of the proposed work include the implementation of relevant chemical kinetics data for high-temperature air and ablation products, the development of an automated grid generation and smoothing tool for hypersonic reentry configurations, and the development of modules to provide properly formatted data for the existing MDA and DoD signature prediction tools. The resulting tool will provide MDA with a robust, efficient and extensible modeling and simulation capability for reentry vehicle radar cross-sections and optical signatures.

* information listed above is at the time of submission.

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