Electrically controlled solid propellant (ECSP), as a novel solid propellant, provides
approaches for intelligent solid propulsion systems due to its on-demand switching on–off …

Much attention has been directed toward the development of electrically controlled solid
propellant (ECSP) as it can implement switched on–off as well as regulation of burning rate …

One of the main goals for the scientific/military rocket industry is to increase the operational
burning time, thus the specific impulse. New homogeneous and heterogeneous propellants …

The regression rate of the solid fuel in the spinning solid fuel ramjet is investigated here
using numerical simulations. The finite volume solver of the reacting turbulent flow is …

This paper aims to introduce a new technique to eliminate the erosive burning phenomenon
in solid rocket motors. The erosive burning which occurs in motors with high volumetric …

In this work, the transient thrust force of the solid propellant rocket motor is numerically
computed to illustrate the shortcomings of the common thrust formula in transient periods of …

Each missile has a payload section and an engine section. In the path of the missile, there is
a time when the mission of the engine section is over and after that the engine will not play …

为了探究HAN 基电控固体推进剂(ECSP) 的电热耦合特性和燃烧性能, 通过改变施加电压和环境
压力对ECSP 进行燃烧性能测试. 在ECSP 燃烧性能测试装置中采用电压 …

In order to explore the electrothermal coupling characteristics and combustion performance
of HAN-based electrically controlled solid propellant (ECSP), the combustion performance …

The selection of controlled parameters of ramjet engine is the foundation of the ramjet
engine control system design. The basic principles for the selection of controlled parameters …