Results show that these two fuels possess a two-stage combustion process.
结果表明，这两种燃料的低温燃烧拥有两阶段放热。
A new modular method for calculating the maximum combustion chamber pressure with stage combustion cycles is proposed in this paper.
提出了一种新的液体火箭发动机分级燃烧循环最高室压计算方法。
The stage combustion cycle using the liquid oxygen and methane as propellant is calculated with the program, and the calculation results are also given.
本文给出了用该程序对采用液氧、丙烷作为推进剂的分级燃烧循环进行计算的结果。
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