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  4. FOX7/GAP rocket propellants for a shoulder launched projectile
 
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2013
Conference Paper
Title

FOX7/GAP rocket propellants for a shoulder launched projectile

Abstract
Several Fox7 based propellant formulations were studied in order to obtain a minimum or reduced smoke composite propellant with inherent IM-properties. Two polymer binder systems are examined: the high energy GAP and a low energy poly-urethane binder containing a large fraction of high energetic plasticizers. Variation of the AP level in the Fox7/GAP propellants gives burn rates of between 10 and 20 mm/s with low pressure exponents. Crawford as well motor-firings of Fox7/AP/GAP formulations indicated a surprising plateau burning behaviour between 7 and 12 MPa, very similar to Double-Base propellants. Chemical stability and sensitivity data demonstrated acceptable values. Fox7/PU compositions with nitro plasticizers exhibit the best thermal stability within ARC measurements. Shock sensitivity test results correspond to values with a 1.3 hazard classification. The conclusion is that Fox7/GAP propellants are suitable for the rocket propulsion of projectiles in shoulder lau nched weapons, although the mechanical properties may need further improvement.
Author(s)
Lips, H.
Menke, K.
Mainwork
27th International Symposium on Ballistics 2013. Proceedings. Vol.1: Interior Ballistics, Exterior Ballistics, Launch Dynamics, Vulnerability & Survivability, Explosion Mechanics  
Conference
International Symposium on Ballistics 2013  
Language
English
Fraunhofer-Institut für Chemische Technologie ICT  
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