摘要
火焰衰减是运载火箭遥测系统设计中的一个重要问题。通过研究火焰衰减建立其数学模型,进行仿真,并分析了各种因素对火焰衰减的影响,为系统设计提供参考。
Flame attenuation is an important factor in the design of the telemetry system of launch vehicles. The model of flare attenuation is founded by researching its theory and validated by simulation, and the different factors which effect the flame attenuation are analysed to give a reference to the system design.
出处
《导弹与航天运载技术》
北大核心
2007年第4期10-12,28,共4页
Missiles and Space Vehicles
关键词
运载火箭
火焰衰减
遥测传输系统
仿真验证
Launch vehicle
Flare attenuation
Telemetry transmission system
Simulation and validation
