The paper presents the composition, functions, technical performance and research of the solid rocketramjet engine ground test equipment and measurement control system in detail.
介绍了固体火箭冲压发动机地面实验装置及测控系统组成、功能、技术指标和可以开展的研究工作。
2
The numerical simulation of turbulent combustion in the afterburner of solid rocketramjet was performed by applying the probability density function non -premixed mode.
应用概率密度函数非预混模型，对固体火箭冲压发动机补燃室内的湍流燃烧进行了数值模拟。
3
This paper discusses operating principles and technology challenges of the integral solid propellant rocketramjet.