DocumentCode :
867850
Title :
Temperature Compensation and Improved Ballistic Performance in a Solid-Propellant Electrothermal-Chemical (SPETC) 40-mm Gun
Author :
Alimi, Roger ; Bakshi, Lior ; Kot, Eran ; Sudai, Moris
Author_Institution :
Propulsion Phys. Div., Soreq Nucl. Res. Center, Yavne´´el
Volume :
43
Issue :
1
fYear :
2007
Firstpage :
289
Lastpage :
293
Abstract :
A solid-propellant electrothermal-chemical (SPETC) 40-mm gun has been designed, constructed, and tested in the indoor firing facilities of the Soreq Propulsion Division Laboratory. An external injector device converts the electric energy stored in the capacitors of the pulse forming network (PFN) into a high-temperature plasma jet that penetrates the gun cartridge and boosts the whole ballistic process. However, unlike large-caliber SPETC systems, in which electric energy is limited to ignition purposes, the 40-mm SPETC gun is a genuine hybrid gun with almost equal electric and chemical contributions. There is experimental evidence that this unique feature induces a very peculiar initial propellant temperature compensation mechanism. It seems that when a significant part of the propelling energy comes from the plasma, i.e., electric energy is not only predominant at the ignition stage of the firing but also later on, then the temperature sensitivity of the propellant tends to vanish. A simple theoretical model supports the experimental findings. The large amount of electric energy is also responsible for a recorded ballistic improvement of 15% in the projectile muzzle kinetic energy. Calibrated simulations show that an optimal tailoring of the power pulse shape and suitable propellant grain geometry should further increase by 10% the muzzle kinetic energy. These modifications are in progress and results should be soon available
Keywords :
ballistics; capacitor storage; design engineering; electrothermal launchers; ignition; plasma jets; 40 mm; Soreq Propulsion Division Laboratory; ballistic process; external rejector device; gun cartridge; indoor firing facilities; initial propellant temperature compensation mechanism; projectile muzzle kinetic energy; pulse forming networks; solid-propellant electrothermal-chemical gun; temperature compensation; temperature sensitivity; Electrothermal launching; Firing; Ignition; Kinetic energy; Laboratories; Plasma chemistry; Plasma temperature; Propulsion; Temperature sensors; Testing; Electrothermal-chemical; plasma injector; temperature compensation;
fLanguage :
English
Journal_Title :
Magnetics, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9464
Type :
jour
DOI :
10.1109/TMAG.2006.887688
Filename :
4033017
Link To Document :
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