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3-D Modeling of Rocket Motor Plumes

Award Information

Agency:
Department of Defense
Branch:
Missile Defense Agency
Award ID:
64290
Program Year/Program:
2004 / SBIR
Agency Tracking Number:
031-1001
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
Combustion Research and Flow Technology, Inc.
6210 Kellers Church Road Pipersville, PA -
View profile »
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
 
Phase 2
Fiscal Year: 2004
Title: 3-D Modeling of Rocket Motor Plumes
Agency / Branch: DOD / MDA
Contract: FA9300-04-C-0044
Award Amount: $748,856.00
 

Abstract:

Characteristics of missile plume signature emissions have a great potential to enhance defensive capabilities in a number of important areas related to early (boost-phase) detection and identification of the missile system/rocket motor. Missile defense technologies where plume modeling plays a significant role include: early warning launch detection (ELDT), post launch warning detection; missile typing algorithms; discrimination; and, background clutter discrimination. The goal of this Phase II effort is the development of a fast-running, engineering plume flowfield model, RPFM-3D, for providing 3D Visible/UV-LWIR/RCS/RF signatures of "real-world" threat missiles with complex features, e.g. gas generators, jet steering vanes and fins, thrust vector control (TVC), etc. Absence of such modeling has hindered maximum exploitation of plume signatures for threat detection and tracking. It will support development & testing of algorithms for hit to kill, "plume to hardbody" handover, aim point selection, etc. The final product of this program will be an engineering-oriented, reliable software tool usable by the boost-phase intercept community. The model will implement innovative Artificial Neural Network techniques in combination with robust numerical algorithms, automatic grid generation and a user-friendly plume-oriented, GUI-driven Expert Interface to provide a rapid turnaround capability within a high throughput, parallel architecture framework.

Principal Investigator:

Neeraj Sinh
Vice President & Technica
2157661520
sinha@craft-tech.com

Business Contact:

Neeraj Sinha
Vice President & Technica
2157661520
sinha@craft-tech.com
Small Business Information at Submission:

COMBUSTION RESEARCH & FLOW TECHNO
6210 Keller's Church Road Pipersville, PA 18947

EIN/Tax ID: 232759059
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No