Chinese translation for "ducted rocket"
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- 冲压火箭复合式发动机
导管火箭
火箭冲压喷气发动机
Related Translations:
- Example Sentences:
| 1. | Study of the unchoked ducted rocket engine and fuel - rich propellant
非壅塞固体火箭冲压发动机及其贫氧推进剂 | | 2. | It is a key technique for ducted rocket to make the second combustor operate at high efficiency and stability
实现补燃室高效率、稳定、可靠的工作，是固体火箭冲压发动机的关键技术问题。 | | 3. | An experimental unchoked ducted rocket motor system is designed in this paper , and some experiments are finished
本文还完成了实验小型非壅塞固体火箭冲压发动机设计，并进行了实验研究。 | | 4. | Mayer a e h j , stowe r a . experimental study into mixing in a solid fuel ducted rocket combustion chamber [ r ] . aiaa 2000 - 3346
余勇,陈小前,等.三维实验固体火箭冲压发动机燃烧室湍流反应流数值模拟[ j ] .国防科技大学学报, 2002 , ( 5 ) | | 5. | In addition , the usaf continues to fund development work of the aerojet ( formerly atlantic research ) variable flow ducted rocket ramjet system as a future propulsion option for an extended range aam
此外，美国空军继续投资于航空喷气研究所（原来的大西洋研究所）的可变喷流管火箭发动机系统，将其作为增程空空导弹的未来推进选项。 | | 6. | In this paper , simple reacting flow model in solid - propellant ducted rocket combustor based on eddy break - up model is established . the model is used to simulate the three - dimensional combustion flowfields in an experimental motor . some factors how to affect the combustion efficiency are discussed in the paper , including air intake and gas generator nozzle
本文基于简单反应的旋涡分裂模型，建立了固体火箭冲压发动机补燃室内的湍流燃烧模型，并在该模型下对某实验发动机进行了三维数值模拟，研究了补燃室设计参数包括进气道出口设计参数和燃气发生器喷管设计参数对燃烧效率的影响。 | | 7. | The solid - propullant ducted rocket , which combines the advantages of solid propullant rocket and ramjet propulsion , is a new kind of combined propulsion system . it offers considerable advantages for missile propulsion , such as high specific impulse , high speed , light weight , long range , high maneuver and simple structure . as the major direction of the propulsion system for supersonic missile , the ducted rocket has good prospects
它将固体火箭技术和冲压技术有机结合在一起，具有比冲高、速度快、重量轻、射程远、机动性能好和结构简单等诸多优点，最大限度地满足了新一代导弹对其动力装置提出的要求，是超声速导弹动力装置的一个主要发展方向，有着广阔的研究前景。 | | 8. | The results showed that the environmental pressure and catalysts have various actions on the thermal decomposition characteristics of the propellant and its ingredients . the burning rates of the gap / tmo fuel - rich propellants were measured by use of the pipe - connected unchoked ducted rocket testing facility
实验结果表明，在不同压强下，贫氧推进剂各组分的热分解特征有所不同；在同一压强下， tmo催化剂对贫氧推进剂中不同组分的催化作用不尽相同；同一催化剂，在不同压强下对同一组分的催化能力也不同。 |
- Similar Words：
- "ducted propeller" Chinese translation, "ducted propulsion unit" Chinese translation, "ducted pulsejet" Chinese translation, "ducted purl" Chinese translation, "ducted radiator" Chinese translation, "ducted rocket propulsion system" Chinese translation, "ducted spinner" Chinese translation, "ducted thruster" Chinese translation, "ducted-fan" Chinese translation, "ducted-fan configuration" Chinese translation
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