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
Price:
$ 50
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
Pages:
9 pages
Scope
This document specifies the general design requirements, detailed design requirements, and other content such as the design basis, design guidelines, design content, and procedures for the discharge of residual propellant from spacecraft.
This document is applicable to the active and passive discharge design of propellants and high-pressure gases in spacecraft. The discharge design of other working fluids on spacecraft can be implemented with reference to this document.
Development Information
Referenced Standards
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