GB/T 31767-2015
Active
GB/T 40536-2021
Active
National standards
GB/T 40536-2021 Design requirements for residual propellant venting of spacecraft
GB/T 40536-2021 Design requirements for residual propellant venting of spacecraft
Basic Information
Standard Code:
GB/T 40536-2021
Standard Type:
National standards
Standard Status:
Active
is_force_gb:
no
CCS Name:
\nSpacecraft power system
ICS Name:
Aerospace engines and propulsion systems
Publish Date:
2021-08-20
Implement Date:
2022-03-01
Publisher:
国家市场监督管理总局、国家标准化管理委员会
Technical Committee:
全国宇航技术及其应用标准化技术委员会(SAC/TC 425)
Pages:
9 pages
Scope
本文件规定了航天器剩余推进剂排放的设计依据、设计准则、设计内容和程序等一般设计要求、详细设计要求等内容。
本文件适用于航天器的推进剂及高压气体的主动排放设计和被动排放设计。航天器上其他工质的排放设计可参照执行。
Development Information
Drafting Units:
北京控制工程研究所
Drafting Persons:
宋涛、梁军强、丁凤林、孙水生、尹文娟、耿永兵、李泽、高俊、林震、李文、张澜
Referenced Standards
Related Standards
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MH/T 9007-2014 Civil aviation engine system component environmental testing guideline
MH/T 9006-2014
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MH/T 9006-2014 A method for calculating the gaseous exhaust emissions from an aero-gas turbine engine
MH/T 6089-2012
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MH/T 6089-2012 Guidelines for monitoring and component management of aviation gas turbine engine lifespan usage
MH/T 3006-2011
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MH/T 3006-2011 Civil aviation maintenance lifting device inspection technical specification
MH/T 3021-2011
Abolished