Minchao Huang, Ph.D., is Professor. He was awarded a Doctorate in Aerospace Science and Technology from National University of Defense Technology (NUDT) in 1998 and a bachelor’s degree in liquid rocket engine from NUDT in 1991. He is mainly engaged in the research of liquid rocket engine, solar thermal propulsion system, and microsatellite precision thrusters. In undergraduate teaching, "Rocket Propulsion Element", "Missile Propulsion Technology", "Engineering Thermodynamics," and "Aerospace Thermal Power Engineering" courses were done from 2005. He has presided over more than 30 national fund projects, aerospace science and technology fund projects, etc. He has won 1 first prize for military science and technology progress, 5 national invention patents, published more than 100 academic papers, 5 academic monographs, and 5 textbooks.

• Section 1 Modeling and simulation analysis of the operation of a space propulsion system.- Chapter 1: Introduction.- Chapter 2: Mathematical model of the operation of the space propulsion system.- Chapter 3: Analysis of the response characteristics of the tank pressurization system and a single thruste.- Chapter 4: Analysis of the response characteristics of coupled multiple thrusters during the working process.- Section 2: Modeling and simulation analysis of the operation of the gel propulsion system.- Chapter 5: Mathematical model of the operation of the gel propulsion system.- Chapter 6: Simulation analysis of the operation of the gel propulsion system.- Section 3: Modeling and Simulation Analysis of the Working Process of the Pumped Liquid Rocket Engine.- Chapter 7: Mathematical model of the operation of a pump-fed liquid rocket engine.- Chapter 8: Simulation analysis of the starting process of the pump-fed liquid rocket engine.