Current position: Home >> Scientific Research >> Paper Publications

Numerical simulation of the start process of a han-based mono-propellant rocket thruster

Release Time:2023-01-07  Hits:

Date of Publication: 2022-10-07

Journal: 68th International Astronautical Congress: Unlocking Imagination, Fostering Innovation and Strengthening Security, IAC 2017

Institution: 运载工程与力学学部

Volume: 2

Page Number: 1244-1250

Prev One:New Contour Design Method for Rocket Nozzle of Large Area Ratio

Next One:Numerical simulation of the transient process of monopropellant rocket engines