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- External Tank Rocket Motor 外挂燃料箱火箭发动机
- The external tank and solid rocket boosters are waiting in the VAB. 航天飞机外贮箱和火箭推进器就在该中心等待装配。
- Space shuttle Atlantis is towed into the Orbiter Processing Facility, or OPF, after being removed from the external tank and solid rocket booster stack. 与外贮燃料箱和固体助推火箭分离后，亚特兰蒂斯号航天飞机回到轨道器处理厂（OPF）保存。
- The shuttle, in contrast, requires three rocket engines built into the vehicle, an external tank of liquid hydrogen and oxygen to feed those engines, and a pair of solid-fuel boosters. 反观太空梭升空则需要使用三具内建的火箭引擎，外附装有液态氢和液态氧的燃料箱，以及一对固体燃料助力器。
- Rocket motor cases and the specially designed production equipment therefor. 四、火箭发动机的壳体及为其专门设计的生产设备。
- External Tank 130 moves out of the Pegasus barge docked at the turn basin at NASA's Kennedy Space Centerin Florida. 佛罗里达州肯尼迪航天中心，130%23外贮燃料箱从飞马座转运驳船的坞中移出。
- Four nozzles, canted outboard, split the exhaust of the solid rocket motor into four equal tails. 四个向外倾斜的喷管把固体火箭发动机的排气流分成四个相等的尾巴。
- There is a rocket motor on the satellite by which the direction of the satellite can be changed if necessary. 在卫星上还有一个火箭马达,必要时可以用它来改变卫星的方向。
- Rocket motors have many advantages over other forms of propulsion. 火箭发动机比其他推进器有许多优点。
- According to the requirement of pasty propellant rocket motor, a composite plasma igniting plan was adopted. 摘要根据膏体推进剂火箭发动机。
- The influence of structure axial vibration on the internal ballistics of solid rocket motor was investigated. 文中研究了固体发动机结构的轴向振动对燃烧室内弹道性能的影响。
- Investigated charring erosive characters of internal insulation of solid rocket motor under flight acceleration. 研究了固体火箭发动机内绝热层在飞行加速度条件下的炭化烧蚀特性。
- The thrust vector control(TVC) performance test of solid rocket motor is presented in this paper. 本文介绍了固体火箭发动机水下推力矢量特性试验。
- Rocket Squads and Mammoth Tank rockets will be tasked to clearing the skies of enemy aircraft, Additionally Rocket Troops can serve as an effective meat-shield. 火箭兵和猛犸得火箭将被用来清空敌人得空军。此外，火箭兵也可以作为有效得肉盾。
- A response surface method(RSM) for structure reliability analysis of solid rocket motor(SRM) grain was presented. 发展了一种固体火箭发动机药柱结构可靠度分析的响应面法。
- The preliminary design data for the k APPA-DX rocket motor is presented in this web page. 初步设计数据的K appa -的DX火箭发动机是在这方面的网页。
- Buckling analysis on rear dome of solid rocket motor case was studied by means of ANSYS. 用ANSYS软件对固体发动机壳体后封头进行了外压屈曲分析。
- Alloy 2219 is very easily weldable and has been extensively welded in fabricating the external tanks for the U.S. space shuttle. 合金2219很容易焊接，已广泛应用于美国航空飞机的外挂油箱的焊接。
- Crose J G.Reliability of solid rocket motor cases and nozzles[R].NTI S,N93-22103. 王松柏.;固体火箭发动机壳体结构的动态可靠性设计[J]
- Finite element method is used in the study of nozzle damping of instable combustion in a solid rocket motor. 应用有限单元法研究固体火箭发动机不稳定燃烧中的喷管阻尼，并用波衰减对比法进行了试验研究。
