火箭推进Rocket Propulsion |
|
课程网址: | http://ocw.mit.edu/courses/aeronautics-and-astronautics/16-512-ro... |
主讲教师: | Manuel Martinez-Sanchez |
开课单位: | 麻省理工学院 |
开课时间: | 2005-01-01 |
课程语种: | 英语 |
中文简介: | 本课程重点介绍发射,轨道和行星际飞行的化学火箭推进系统。它研究了固体,液体双组元推进剂和混合火箭发动机的建模。还将涵盖热化学,特定脉冲的预测以及包括真实气体和动力学效应的喷嘴流。其他主题包括结构限制,推进剂进料系统,涡轮泵以及固体,液体和混合火箭的燃烧过程。 |
课程简介: | This class focuses on chemical rocket propulsion systems for launch, orbital, and interplanetary flight. It studies the modeling of solid, liquid-bipropellant, and hybrid rocket engines. Thermochemistry, prediction of specific impulse, and nozzle flows including real gas and kinetic effects will also be covered. Other topics to be covered include structural constraints, propellant feed systems, turbopumps, and combustion processes in solid, liquid, and hybrid rockets. |
关 键 词: | 火箭推进系统; 混合火箭发动机; 结构约束; 推进剂供给系统; 涡轮泵 |
课程来源: | 麻省理工学院公开课 |
最后编审: | 2020-11-30:yumf |
阅读次数: | 64 |