Effects of Hardbody-Plume Interactions on Radar Returns

Award Information
Agency: Department of Defense
Branch: Missile Defense Agency
Contract: HQ0006-10-C-7310
Agency Tracking Number: B093-031-0110
Amount: $99,995.00
Phase: Phase I
Program: SBIR
Awards Year: 2010
Solicitation Year: 2009
Solicitation Topic Code: MDA09-031
Solicitation Number: 2009.3
Small Business Information
6210 Kellers Church Road, Pipersville, PA, 18947
DUNS: 929950012
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Vineet Ahuja
 Senior Research Scientist
 (215) 766-1520
Business Contact
 Brian York
Title: Principal Scientist & Treasurer
Phone: (215) 766-1520
Email: york@craft-tech.com
Research Institution
The innovation in this proposal relates to the use of a generalized framework for prediction of RCS that utilizes a common procedure for computing the signature from a hardbody and its associated plume. The RCS methodology is based on a first principles approach to the solution of the Maxwell’s equations utilizing a Vector Finite Element Method. The framework can be readily applied to predict the RCS signatures for complex three-dimensional hardbody configurations that include fins, multiple nozzles, etc. as well as highly asymmetric plumes that result from missiles flying at an angle of attack and structural interactions of the missile body and plume. Detailed studies will be performed that look at the interference effects of the hardbody, its structural components and the associated plume. Combined hardbody/plume simulations for configurations of interest will be performed and the sensitivity of the integrated RCS signature to hardbody-plume interactions will be evaluated in this proposal.

* Information listed above is at the time of submission. *

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