研究了整体式固体火箭冲压发动机的应用性能。
Applications of integral solid propellant rocket ramjets arc researched.
推力调节是整体式固液火箭冲压发动机研究的一项关键技术。
Thrust regulation is a key technology on the solid liquid rocket ramjet engine.
首先建立研究静止增程固体火箭冲压发动机补燃室燃烧特性的物理和数学模型。
Physical and mathematic model of investigating combustion characteristics of secondary combustion chamber for static extended solid rocket ramjet was established.
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