Investigations on Internal Ballistic Characteristics of Pasty Propellant Rocket Engine
Pasty rocket engines have broad application prospects in the aerospace field. To study the internal ballistic characteristics of the pasty propellant rocket engine, the burning surface change model of pasty propellant was built. The calculation program was developed to calculate the pressure evoluti...
Saved in:
Main Authors: | Xinyou Shan, Yingkun Li, Xiong Chen, Yan Wu, Yong He, Weixuan Li |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2021-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2021/9952209 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Analysis of Thermal Decomposition of Solid Rocket Propellants
by: Marcin CEGŁA, et al.
Published: (2019-06-01) -
Mechanical Compression Behaviour of "Green" Rocket Propellants
by: Florin M. DÎRLOMAN, et al.
Published: (2023-06-01) -
Thermal loading of spent rocket stage structure during ballistic descent
by: V. Yu. Kudentsov, et al.
Published: (2022-03-01) -
Development and analysis of simulation of liquid-propellant rocket engine pump head curve obtaining process
by: D. A. Savchin, et al.
Published: (2021-03-01) -
Investigation of properties of system of automatic control of liquid-propellant rocket propulsion system with integrating regulator
by: I. A. Kyzmenko, et al.
Published: (2019-03-01)