发明名称 Missile with propulsion plug - has guide bush for gases to tracer charge in plug shutting off gap
摘要 The missile with propulsion plug has a tracer charge in its body and an ignition passage in the plug directing the propulsion gases at the charge on firing, while a gap is left between plug and body. A bush is inserted in the passage and/or the tracer charge recess, directing the gases straight at the tracer charge. Thus shuts off the gap between passage and recess on firing. ADVANTAGE - No gas escape occurs through the gap.
申请公布号 DE4038782(A1) 申请公布日期 1992.06.11
申请号 DE19904038782 申请日期 1990.12.05
申请人 MAUSER-WERKE OBERNDORF GMBH, 7238 OBERNDORF, DE 发明人 REUTER, INGOLF, DIPL.-ING., 7242 DORNHAN, DE;HEZEL, ULRICH, DIPL.-ING.;REUTER, KLAUS-PETER, DIPL.-ING., 7230 SCHRAMBERG, DE
分类号 F42B12/38;F42B14/06 主分类号 F42B12/38
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