The author considers that adopting the helium pressurization can decrease greatly the engine pump inlet pressure of the upper stage rocket, and considerably increase transport capacity of the rocket.

 
  • 認為采用氦氣增壓,我國可貯存推進(jìn)劑上面級火箭發(fā)動(dòng)機氧化劑泵入口壓力要求可以大幅度地降低,較大地提高火箭的運載能力。
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