发明名称 PROCEDIMIENTO PARA FABRICAR UN PERFORADOR PARA UN PROYECTIL CON JAULA PROPULSORA
摘要 <p>Missile made from hard metal, such as W or U comprises a penetrator, a drive cage and an aerodynamic hood whereby the penetrator from front area to stern is made as one part. The penetrator in its middle region has a lower strength and higher toughness than in the front region and the stern region has a higher strength and lower toughness than in the middle region and a lower strength and higher toughness than in the front region.</p>
申请公布号 ES545086(D0) 申请公布日期 1987.10.16
申请号 ES19860005450 申请日期 1985.07.11
申请人 VOEST ALPINE AKTIENGESELLSCHAFT 发明人
分类号 (IPC1-7):F42B13/04 主分类号 (IPC1-7):F42B13/04
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