Dynamic Behavior of Nano-sized Particles in Novel Energetic Materials for Space Propulsion

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$99,135.00
Award Year:
2009
Program:
STTR
Phase:
Phase I
Contract:
FA9550-09-C-0012
Agency Tracking Number:
F08A-010-0107
Solicitation Year:
2008
Solicitation Topic Code:
AF08-T010
Solicitation Number:
2008.A
Small Business Information
ILLINOISROCSTAR LLC
P. O. Box 3001, Champaign, IL, 61826
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
792045713
Principal Investigator:
William Dick
CEO & Managing Member
(217) 417-0885
wdick@illinoisrocstar.com
Business Contact:
Michael Ludwig
Associate Director
(765) 494-1055
mrludwig@purdue.edu
Research Institution:
PURDUE UNIV.
Mike Ludwig
Sponsored Program Services
302 Wood Street
West Lafayette, IN, 47907 2108
(765) 494-1055
Nonprofit college or university
Abstract
We propose a comprehensive computational and experimental program to investigate the charac-teristics and dynamic behavior of nano-size aluminum in novel energetic materials. Two classes of advanced propellants will be considered. The first will be composite propellants, consisting of solids including AP, HMX, RDX, or nano-aluminum with a suitable binder such as HTPB. The second will be a nanoscale aluminum and ice propellant. For the computational portion of the proposed work, we plan to (i) use our in-house packing code to generate morphologies of interest for heterogeneous propellants; (ii) modify our CFD code to include appropriate models for chemistry, radiation, and nano-sized aluminum; and (iii) simulate transient behavior of the pro-pellants at rocket motor conditions. For the experimental portion, we plan to (i) use the mixing facility at Purdue to prepare appropriate propellant samples containing nano-sized aluminum, thus allowing for a full characterization of the propellant (composition; particle size distribution) necessary for a coordinated modeling and experimental program; and (ii) carry out both steady and unsteady experiments to fully characterize the propellants. The experiments will also be used for model calibration and for validation.

* information listed above is at the time of submission.

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