GB/T 32295-2015
ActiveDesign requirements for residual propellant venting of launch vehicle
运载火箭剩余推进剂排放设计要求
Application Summary AI generated
This standard specifies the design requirements for safely venting residual propellant from launch vehicle stages after engine shutdown or mission completion. It is applied in the aerospace industry for the development and testing of liquid-propellant rockets, ensuring that residual fuels and oxidizers are expelled in a controlled manner to prevent explosion risks, contamination, or uncontrolled re-entry hazards. The standard guides engineers in designing venting systems for both orbital and suborbital launch vehicles.
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