标准简介
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 stages.Residual propellant disposition design for independent upper stages can refer to this standard.英文名称：Design requirements for residual propellant venting of launch vehicle
标准状态：现行
中标分类：航空、航天>>航天器及其附件>>V71航天器总体
ICS分类：航空器和航天器工程>>49.020航空器与航天器综合
发布部门：General Ad.
发布日期：2015-12-31
实施日期：2016-07-01
出版日期：2018-06-01
页数：12页
前言
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