<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
IT1174260(B)
申请公布日期
1987.07.01
申请号
IT19780069960
申请日期
1978.12.28
申请人
THE SECRETARY OF STATE FOR DEFFENCE IN HER BRITANNIC MAJESTY'S GOVERMENT OF THE
