The invention provides a rocket takeoff method which is applied to a rocket takeoff stage, and compared with an existing takeoff process, the method does not need working processes such as propellant replenishing, engine pre-cooling and pressurized gas replenishing.
本发明提供了一种火箭起飞方法,该方法应用在火箭起飞阶段,相比现有起飞流程,该方法不需要推进剂补加、发动机预冷、增压气体补加等工作流程。
Rocket take-off method
一种火箭起飞方法
2024-05-03
Patent
Electronic Resource
Chinese
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