6秒之后，航天飞机的双固体燃料火箭推进器点火，固定航天器的爆炸螺栓切断，整个航天飞机一飞冲天。
After those six seconds, a shuttle? S twin solid rocket boosters ignite, explosive bolts holding the spacecraft down are severed and the entire stack soars spaceward.
利用基元反应机理数值模拟了H2／空气良好搅拌反应器（CSTR）系统的双稳定状态和点火过程。
The bistable states and ignition in an H2/air CSTR (continuous-flow stirred tank reactor) are numerically simulated based on the detailed chemistry.
直接点火线圈，双电极火花塞和高输出的磁提供极其精确，可靠的点火。
Direct ignition coils, dual-electrode spark plugs and high-output magneto deliver extremely accurate, reliable firing.
为了改善电喷汽油机冷起动及冷态怠速运转（即暖车过程）性能，自行研制了基于高能双火花塞点火的快速燃烧系统。
Improvement of cold starting and cold idling circulation(engine warming up)combustion process of motorcycle gasoline engines by dual-spark plug-based rapid burning system was introduced.
采用气氧作氧化剂、气氢作燃料，对具有高度补偿特性的塞式喷管和双钟型喷管进行了点火热试。
By employing the gaseous oxygen as oxidizer and gaseous hydrogen as fuel, hot-firing tests were performed for aerospike nozzle and dual-bell nozzle test engines with altitude compensating features.
通过分析研究点火瞬态过程中推进剂内部急速热传导存在的非傅立叶效应，推导得到具有双曲性质的固体推进剂瞬态热传导方程。
After affirming the existence of non-Fourier effect, the hyperbolic equation suited for describing rapidity heat transfer process inside propellant is obtained.
等离子点火技术应用于双进双出磨直吹式制粉系统时，能满足等离子点火浓度的技术及运行实况。
Plasma ignition technology is applied to a dual-in dual-out direct-fired system, which satisfied pulverized-coal concentration requirements and practical operating conditions.
等离子点火技术应用于双进双出磨直吹式制粉系统时，能满足等离子点火浓度的技术及运行实况。
Plasma ignition technology is applied to a dual-in dual-out direct-fired system, which satisfied pulverized-coal concentration requirements and practical operating conditions.
应用推荐