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GB/T 32295-2015 Active
GB/T 32295-2015 Design requirements for residual propellant venting of launch vehicle
Abstract
This standard specifies the design criteria for the discharge of residual propellant from the last stage of a launch vehicle during flight, the selection of discharge methods, and other general design requirements, detailed design requirements, and effect evaluations. This standard applies to the design of discharging residual propellant from the last stage of launch vehicles using room-temperature liquid propellants and cryogenic liquid propellants. The design related to the discharge of residual propellant from the upper stage of launch vehicles and other parts can be implemented with reference to this standard.
General Product Information
| Document Type | National standards |
|---|---|
| Standard Status | Active |
| Standard Code | GB/T 32295-2015 |
| CCS | The overall structure of the spacecraft |
| ICS | Integrated aircraft and spacecraft |
| Implement Date | 2016-07-01 |
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