The optimization model is setup with the minimum takeoff mass. On this basis. a large-scale software IDAMS is made. which can be used to optimize the system. ballistic and SRM parameter simultaneously.
以起飞质量最小为目标函数建 立了优化模型，并编制了大型总体／发动机一体化设计软件IDAMS，可对总体参数、弹 道参数和发动机参数同时优化。
参考来源 - 飞行器总体优化设计理论与应用研究·2,447,543篇论文数据，部分数据来源于NoteExpress
Assumed temperature is the equivalent ambient air temperature determined by the actual takeoff mass of an aircraft.
假设温度是由飞机实际起飞质量确定的相当的大气温度。
Under the conditions of the given payload and the highest launching height, the design parameters of the propulsion system are selected to minimize takeoff mass of the rocket.
在给定有效载荷、最高射高的条件下，选取动力系统的设计参数使火箭的起飞质量最小。
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