DocumentCode :
1348336
Title :
Recent advances in electrothermal-chemical gun propulsion at United Defense, L.P
Author :
Chaboki, A. ; Zelenak, S. ; Isle, B.
Author_Institution :
Armament Syst. Div., United Defense, Minneapolis, MN, USA
Volume :
33
Issue :
1
fYear :
1997
fDate :
1/1/1997 12:00:00 AM
Firstpage :
284
Lastpage :
288
Abstract :
Electrothermal-chemical (ETC) propulsion uses an electrical energy pulse as a means of initiating and, in some cases, controlling the combustion of propellant charges. The electrical energy pulse is generated by a pulse-forming network (PFN) and is dissipated within the gun in the form of a plasma. The high-energy density plasma resulting from the electrical energy dissipation has been demonstrated to be highly effective in ignition of solid and liquid propellant charges. Variations in electrical dissipation rate have been shown to affect propellant gasification rate and, therefore, pressurization throughout the ballistic cycle. This paper discusses recent development results at United Defense, L.P., in the areas of ETC solid propellant ignition and performance improvement, ETC temperature compensation, and a high-performance hybrid liquid/solid propellant ETC charge
Keywords :
electrothermal launchers; ballistic cycle; combustion; electrical energy pulse; electrothermal-chemical gun propulsion; energy dissipation; gasification; hybrid liquid/solid propellant charge; plasma energy density; pressurization; pulse-forming network; solid propellant ignition; temperature compensation; Combustion; Electrothermal effects; Electrothermal launching; Energy dissipation; Ignition; Plasma density; Plasma temperature; Propulsion; Pulse generation; Solids;
fLanguage :
English
Journal_Title :
Magnetics, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9464
Type :
jour
DOI :
10.1109/20.559970
Filename :
559970
Link To Document :
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