solid propellants rocket 固体火箭发动机
Burning rate measurement with closed burner is a rapid method for measuring burning rate character and its change of solid rocket propellants in a wide pressure range.
密闭燃烧器法是一种能测定很宽压强范围内固体火箭推进剂燃速特性及变化情况的快速测量方法。
However, from what I gather, "hybrid" rocket engines use both solid and liquid or gas propellants.
然而我的理解是，“混合动力”火箭引擎同时使用固体燃料和液态或气态推进剂。
The spaceship will be fuelled by a "hybrid rocket" -so-called because it contains both liquid and solid propellants.
飞船将使用液体与固体混合的助推剂作为燃料。
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