It has very extensive application prospects because it can realize thrust regulation and multi-time ignition that solid propellant couldn\'t, and also can overcome the disadvantages of liquid propellant\'s danger and engine structure\'s complexity.
膏体推进剂是一种新型的化学火箭推进剂,同时具有固体推进剂和液体推进剂的优点,既能实现固体推进剂无法实现的推力调节和多次点火,又克服了液体推进剂危险性大、发动机结构复杂等缺点,具有广泛的应用前景。
Based on the adiabatic approximation theory,we obtain the approximate expressions of the firing rate (FR),the probability distribution of the first fire (FPD),and the coefficient of variation (CV) of interspike interval of firing.
基于绝热近似理论,得到了神经元首次点火概率分布、神经元点火率和神经元点火峰峰间隔的变差系数的近似表达式。
