GB/T32295-2015E运载火箭剩余推进剂排放设计要求（英文版）

This standard specifies requirements of residual propellant post-mission venting for launch vehicle orbital stages,including general requirements such as design norms and solution selection as well as detailed design requirements and effect evaluation etc This standard applies to residual storable/cryogenic liquid propellant post-mission venting design of launch vehicle orbital stagesResidual propellant disposition design for independent upper stages can refer to this standard

标准号：GB/T 32295-2015E

标准名称：运载火箭剩余推进剂排放设计要求（英文版）

英文名称：Design requirements for residual propellant venting of launch vehicle

标准类型：国家标准

标准性质：推荐性

标准状态：现行

发布日期：2015-12-31

实施日期：2016-07-01

中国标准分类号（CCS）：航空、航天>>航天器及其附件>>V71航天器总体

国际标准分类号（ICS）：航空器和航天器工程>>49020航空器与航天器综合

归口单位：SAC/TC 425,National Technical Co

发布单位：General Ad