Effects of Hardbody-Plume Interactions on Radar Returns

Award Information
Agency:
Department of Defense
Branch
Missile Defense Agency
Amount:
$999,953.00
Award Year:
2011
Program:
SBIR
Phase:
Phase II
Contract:
HQ0147-11-C-7709
Agency Tracking Number:
B2-1758
Solicitation Year:
2009
Solicitation Topic Code:
MDA09-031
Solicitation Number:
2009.3
Small Business Information
Combustion Research and Flow Technology,
6210 Kellers Church Road, Pipersville, PA, -
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
929950012
Principal Investigator:
Neeraj Sinha
Senior Research Scientist
(215) 766-1520
sinha@craft-tech.com
Business Contact:
Brian York
Principal Scientist&Tre
(215) 766-1520
york@craft-tech.com
Research Institution:
Stub




Abstract
Characteristics of missile plume RCS have a great potential to enhance defensive capabilities in several areas related to Ballistic Missile Defense Systems (BMDS). Supporting MDA"s engineering applications related to missile typing, discrimination, tracking, algorithm development, etc. requires estimation of many parameters by the plume models, which can be very expensive for complex targets that are not easily measured. High-fidelity, 3D plume modeling of threat systems is now at an advanced stage, utilizing a MDA-sponsored highly efficient, 3D CFD plume models; however, comparable capabilities are not available for corresponding RCS predictions. The Phase II will demonstrate an advanced 3D Vector Finite Element (VFE) RCS model for performing RCS predictions of 3D effects in plumes, which can strongly shift the Doppler spectrum of the plume from the hardbody return. The Phase II will demonstrate this 3D plume RCS modeling tool as mature for supporting production-oriented analysis, with applicability to the tracking of post-burnout debris for solid motors also.

* information listed above is at the time of submission.

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