Single igniting solid fuel air explosives (FAE) is discussed in the paper. The curves of change of overpressure and specificimpulse with distance are got by experiment.
讨论一次引爆FAE燃料配方，实验测定了空气冲击波超压和冲量随距离的变化曲线。
2
The relations of thrust and specificimpulse to inlet air flow and temperature are derived from theoretical analysis of solid fuel ramjet (SFRJ) performance.
在固体燃料冲压发动机性能分析基础上，推导了某发动机的推力和比冲与入口流量和温度之间的关系式。
3
Theoretical research on specificimpulse performance and chamber length of hydroreactive metal fuel motor;