Experimental set-up and results of the process of co-extruded perforated gun propellants Martijn Zebregs, Chris van Driel [email protected] TNO Defence, Security and Safety – Protection, Munitions and Weapons – Energetic Materials Chris van Driel Introduction • Co-layered gun propellants – advantages and difficulties • Performance characteristics • Co-extrusion of gun propellants at TNO • Experimental set-up • Development steps in recent years • Burning characteristics of 1-perf co-extruded co-layered propellant • Future developments • Conclusive remarks 2 Co-extrusion of gun propellants IM/EM Symposium, Tucson, AZ, May 2009 Co-layered propellants • US Patent 4581998 (1986) A.W. Horst et al. • Advantage: improvement of gun performance by enlargement of the impulse on the projectile • Ritter ICT 2007 Manufacture: • Disadvantage: ‘The time-consuming manufacturing of assembled propellant sheets proved to be a difficult task.’ • TNO’s approach: co-extrusion with proper die design easy manufacturing (not labour intensive and excellent geometries in one step) 3 Co-extrusion of gun propellants IM/EM Symposium, Tucson, AZ, May 2009 Co-layered propellants Advantages Notes • Increased performance • Increased performance of sheet • High progressivity of propellants is comparable to the co-extruded 0- and 1-perf grains performance of regular granular • Decreased erosivity of high multi-perforated propellant energy propellants • Variations in layer thickness may • Increased ignition behaviour result in increased dispersion of V 0 (e.g. LOVA propellants) • Contrary to co-layered sheet propellants, co-extruded propellants provide wide variation in geometries, implying a larger number of possible applications Ritter, ICT 2007 (note: not multi-perforated grains!) 4 Co-extrusion of gun propellants IM/EM Symposium, Tucson, AZ, May 2009 Co-layered propellants • Examples of simulated performance effects 7-perf versus 0-perf co-layered sheet propellant 350 1200 300 1000 250 800 P 7-perf ] Pa] 200 600 m/s P 0-perf P [M 150 400 V(0) [ TT 70--ppeerrff. 100 50 200 0 0 0 0.005 0.01 0.015 Time [s] Ritter, ICT 2007 5 Co-extrusion of gun propellants IM/EM Symposium, Tucson, AZ, May 2009 Performance characteristics • Examples of simulated performance effects 7-perf; T (core) = 3515 K; T (layer) = 3170 K f f factor burning rates = 1.5 350 1200 350 4500 pressure pressure 300 1000 300 4000 ] s gas temperature MPa] 220500 680000 tile) [m/ MPa] 220500 33050000 s) [K] P [ 150 400 ojec P [ 150 2500 T(ga 100 r 100 2000 p 50 projectile 200 V( 50 1500 velocity 0 0 0 1000 0 0.005 0.01 0.015 0 0.005 0.01 0.015 Time [s] Time [s] P conv. P co-layer T conv. T co-layer P conv. P co-layer T conv. T co-layer T = 3165 K max = 3385 K without ‘cool’ outer layer 6 Co-extrusion of gun propellants IM/EM Symposium, Tucson, AZ, May 2009 Performance characteristics • Examples of simulated performance effects 7-perf; T (core) = 3515 K; T (layer) = 2900 K f f factor burning rates = 2 350 1200 350 4500 pressure pressure 300 300 4000 1000 ] s gas temperature MPa] 220500 680000 tile) [m/ MPa] 220500 33050000 s) [K] P [ 150 400 ojec P [ 150 2500 T(ga 100 r 100 2000 p 50 projectile 200 V( 50 1500 velocity 0 0 0 1000 0 0.005 0.01 0.015 0 0.005 0.01 0.015 Time [s] Time [s] P conv. P co-layer T conv. T co-layer P conv. P co-layer T conv. T co-layer T = 3040 K max = 3385 K without ‘cool’ outer layer • Higher charge densities further performance improvement 7 Co-extrusion of gun propellants IM/EM Symposium, Tucson, AZ, May 2009 Performance characteristics • Examples of simulated performance effects Dynamic vivacity 1-perf grain: (both layers intact until Z = 100%) 3 ] u. 2.5 a. [ no layer y t 2 ci va r(core)/r(layer) = vi 1.5 1.5 (sim.) c mi 1 r(core)/r(layer) = na 2 (sim.) y 0.5 D 0 0 0.2 0.4 0.6 0.8 1 P/P(max) [-] increased progressivity, even without double peak; ‘low’ (usual) pressure exponent with smaller outer layer: progressive + double peak in P-time curve large grains (applicable for both medium and large calibre) 8 Co-extrusion of gun propellants IM/EM Symposium, Tucson, AZ, May 2009 Co-extrusion of co-layered propellants at TNO 2 barrels double barrel capillary rheometer heating zones pressure transducers (co-)extrusion block 9 Co-extrusion of gun propellants IM/EM Symposium, Tucson, AZ, May 2009 Co-extrusion of co-layered propellants at TNO First attempts (2005-2006): • Non-perforated co-extruded propellant • ‘Self-encapsulation’ is theoretically possible for a large viscosity difference (factor 2.5), but appears to fail • Improper die design leads to slip, resulting in a ‘rope of beads’ • Experiments resulted in good insight in the problem of co-extrusion 10 Co-extrusion of gun propellants IM/EM Symposium, Tucson, AZ, May 2009