发明名称 Propellant charge for tubular weapon with main and transfer charges
摘要 Tubular weapon includes a main charge (3) which burns normally at about 21 deg C, slower at lower temperatures and faster at higher temperatures. A transfer charge (5) is provided, which exhibits opposite characteristics to the main charge, i.e. burns faster at lower temperatures. Preferably, the max. gas pressure level off the propellant charge (1) when initiated through the transfer charge is approximately constant at any temperature between -40 deg C and +40 deg C. The transfer charge preferably consists of porous propellant charge powder containing air inclusions. The inverse burning characteristic may be induced by incorporation of spherical nitroguanidine or diatomaceous earth.
申请公布号 DE19635795(A1) 申请公布日期 1998.03.05
申请号 DE19961035795 申请日期 1996.09.04
申请人 RHEINMETALL INDUSTRIE AG, 40882 RATINGEN, DE;WNC-NITROCHEMIE GMBH, 84544 ASCHAU, DE 发明人 BOECKER, JUERGEN, DIPL.-PHYS. DR., 46049 OBERHAUSEN, DE;FRYE, GUENTER, 40699 ERKRATH, DE;RAHNENFUEHRER, ECKHARD, DIPL.-PHYS., 41541 DORMAGEN, DE;KRATZSCH, KLAUS-ACHIM, DIPL.-PHYS. DR., 40668 MEERBUSCH, DE;VASATKO, HARTMUT, DIPL.-PHYS. DR., 84478 WALDKRAIBURG, DE
分类号 C06B45/00;C06B45/12;F42C19/08;(IPC1-7):C06B45/00;C06D5/00;C06B45/02;F42B5/16;F42B5/38;F42B12/08 主分类号 C06B45/00
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