发明名称 PROJECTILE TAIL FIN UNITS
摘要 <p>A projectile component is provided with a thermally ablative coating capable of giving complete protection against the erosive effects of in-bore and in-flight heating, with minimal impairment of aerodynamic performance.</p>
申请公布号 GB1604865(A) 申请公布日期 1981.12.16
申请号 GB19770054200 申请日期 1977.12.29
申请人 DEFENCE SECRETARY OF STATE FOR 发明人
分类号 F42B10/06;(IPC1-7):42B13/00;32B33/00 主分类号 F42B10/06
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