发明名称 ROCKET IN-TUBE SPIN DEVICE AND REAR SABOT
摘要 <p>A spin device attached to the rocket nozzle to impart a relatively large amount of spin to the rocket in a short time while the rocket is guided in a tube launcher of a rearward facing step internal configuration. The device also acts as a rear shoe or ???? for the rocket. Upon contact with the rearward facing step, the spin device separates from the rocket. The forward rocket ???? leave the guidance of the forward tube at the same instant of device ?? parall?? thus providing a nonti???old rocket launch</p>
申请公布号 CA1148754(A) 申请公布日期 1983.06.28
申请号 CA19820407794 申请日期 1982.06.21
申请人 UNITED STATES (GOVERNMENT OF THE) AS REPRESENTED BY THE SECRETARY 发明人 BATSON, JAMES L.;BOOKER, DAVID L.
分类号 F02K9/97;(IPC1-7):F02K9/97 主分类号 F02K9/97
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