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ATMOSPHERE RE-ENTRY CAPSULE

机译:大气重入胶囊

摘要

PURPOSE: To contrive to reduce aerodynamic heating at the time of re-entry of an atmosphere re-entry capsule and to provide good aerodynamical motion characteristic at the time of low-level flying using a device exposed after sublimation of an ablation material by covering the ablation material with a low- level flying aerodynamic device provided on the periphery. ;CONSTITUTION: A capsule peripheral protrusion 11 is fitted to the periphery of a capsule body 1 as a low-level flying aerodynamic device. An ablation material 2 is coated on the capsule body 1 and the capsule peripheral protrusion 11 so as to cover them by the thickness decreasing at the time of re-entry. Thus amount of aerodynamic heating at the time of re-entry can be reduced by the effect of the ablation material 2 and the capsule peripheral protrusion 11 can be fuctioned as a low-speed flying aerodynamic device even at the time of low-speed flying.;COPYRIGHT: (C)1996,JPO
机译:目的:通过使用消融材料升华后覆盖的装置,试图减少大气再入舱再次进入时的空气动力加热,并在低空飞行时提供良好的空气动力运动特性。消融材料,其外围设有低空飞行气动装置。组成:胶囊外围突起11安装在胶囊主体1的外围,作为低空飞行的空气动力学装置。消融材料2被涂覆在胶囊主体1和胶囊周缘突起11上,以便通过再次进入时减小的厚度覆盖它们。因此,由于消融材料2的作用,可以减少再次进入时的空气动力学加热的量,并且即使在低速飞行时,胶囊外围突起11也可以作为低速飞行空气动力学装置而起作用。 ;版权:(C)1996,日本特许厅

著录项

  • 公开/公告号JPH08175499A

    专利类型

  • 公开/公告日1996-07-09

    原文格式PDF

  • 申请/专利权人 MITSUBISHI ELECTRIC CORP;

    申请/专利号JP19940324977

  • 发明设计人 KUROTAKI TAKUJI;KUROSAKI RYUJIRO;

    申请日1994-12-27

  • 分类号B64G1/58;B64G1/62;

  • 国家 JP

  • 入库时间 2022-08-22 03:59:57

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