Russian flight controllers conduct thruster tests with the Progress to gather engineering data until it deorbited and burned up in Earth's atmosphere over the Pacific Ocean.
俄国的飞行控制员一直在执行着「进步号」的推进测试来获取引擎的数据,直到它脱离轨道并在太平洋上空的地球大气上燃烧殆尽。
More visible thruster particles.
更明显的推进器粒子。
Rocket Sewage This nitrous oxide-powered rocket thruster designed at Stanford can also be used in a sewage treatment plant to reduce greenhouse gas emissions. Stanford University.
火箭污水处理系统。这个由斯坦福大学研究设计的以氧化氮为动力的火箭推进器,也可用于污水处理工厂以减少温室气体排放。斯坦福大学。
Hovercraft is a kind of high-powered watercraft. the propulsion system of hovercraft concludes mainframe power transfer device thruster air propeller installation and assistant system.
气垫船动力装置由如下各部分组成:主机,功率传输装置,推进器,主推进器舵组合装置,垫升装置以及为动力装置服务的系统和装置。
Rocket sewage This nitrous oxide-powered rocket thruster designed at Stanford can also be used in a sewage treatment plant to reduce greenhouse gas emissions.
火箭污水处理系统。这个由斯坦福大学研究设计的以氧化氮为动力的火箭推进器,也可用于污水处理工厂以减少温室气体排放。
This boat is equipped with one bow thruster for position keeping while fire fighting has good viewing tactical turning performance.
本船艏部设有艏侧推装置,消防时可保持船舶定位,并具有良好的视野和回转性能。
NASA developed a similar engine for its Deep Space 1 Mission, launched in 1998, but the new thruster has advantages.
NASA在1998年所发射的「深空一号」也曾使用类似的引擎,但相较而言,这个新型的推进器有自己的优势。
The department of satellite design and the staff on the ground have conducted a way of thruster calibration execution in terms of the data of the attitude and the nutation principle.
卫星设计部门和地面工作人员根据卫星的特点,利用姿态数据及章动原理建立了一套标定推力器对称性的方法。
A working ion thruster was built by Harold R. Kaufman in 1959 at the NASA Glenn facilities.
离子推进器是一个工作所建哈罗德河考夫曼于1959年在美国航天局格伦设施。
But safety rules prohibit the ships from remaining in space for more than 200 days, since their batteries can lose power and corrosive thruster fuel can degrade rubberized seals.
安全守则规定这些飞船不能暴露在宇宙空间中超过200天,因为电池会流失能量和推进器燃油会腐蚀橡胶密封。
The ion energy distribution in the plasma exhaust plume of a hall thruster is important to evaluate the influence of the hall thruster plume and optimize the thruster position on the spacecraft.
霍尔推力器羽流中的离子能量分布情况对于评估推力器羽流影响,优化推力器在航天器上的布局具有重要意义。
The thruster design requires that the total volume of the propulsion system be less than 10 percent of the CubeSat.
这个推进器设计规定了推进器系统的总体积不超过立方体卫星的10%。