| 1. | The components of solid propellants are of necessity highly reactive and essentially incompatible .
固体推进剂成分必须是很活泼的，基本上是不相容的。 |
| 2. | Solid propellant engine systems are basically less flexible in operation than liquid or hybrid propellant systems .
固体推进剂发动机系统的可调性基本上比液体或混合型的要差。 |
| 3. | A variety of mechanical surfaces have been employed for deflecting the exhaust jets of solid-propellant rockets .
人们已经用过各种类型的机械控制面来偏转固体推进剂火箭的排气流。 |
| 4. | We shall try by means of a highly simplified development to expose certain advantages and disadvantages of solid propellant rocket systems .
我们想通过相当简单的推导来试图阐明固体推进剂火箭系统的某些优缺点。 |
| 5. | Nomenclature of composite solid propellant and charge
复合固体推进剂及装药术语 |
| 6. | Current situation and trend of solid propellant technology abroad
国外固体推进剂技术现状和发展趋势 |
| 7. | A mass of solid propellant
块状燃料一块固体推进剂 |
| 8. | Study on modeling and features of solid propellant air - turbo - rocket
固体推进剂吸气式涡轮火箭发动机的建模及特征研究 |
| 9. | Numerical simulation of deflagration - to - detonation transition in high energy propellant
高能固体推进剂燃烧转爆轰的数值模拟 |
| 10. | Closed burner method is used for determining burning rate of the solid propellants
密闭燃烧器法是一种间接测定固体推进剂燃速的方法。 |
