发明名称 INFLATABLE DECELERATOR
摘要 <p>INFLATABLE DECELERATOR The present invention relates to a collapsible decelerator for aerial bombs launched from a high velocity vehicle and designed to provide a high drag stabilizer capable of withstanding release in airstream velocities moving at 2,600 feet per second. The deceleration includes a hollow inflatable star, the outermost points of which have hooded valve openings through which regulated airflow enters and inflates the star to decelerate the munition to which it is attached.</p>
申请公布号 CA1231861(A) 申请公布日期 1988.01.26
申请号 CA19850498774 申请日期 1985.12.30
申请人 AEROJET-GENERAL CORPORATION 发明人 ZACHARIN, ALEXEY T.
分类号 B64D1/04;B64D17/80;F42B10/48;(IPC1-7):F41F5/02 主分类号 B64D1/04
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