A thrust nozzle for a hypersonic engine

• 1. 电磁型高超音速推力矢量喷气发动机 [P] . 中国专利： CN113513428A . 2021-10-19
• 2. 具有格栅式推力反向器和可变几何喷嘴的用于飞行器发动机的机舱 [P] . 中国专利： CN102844238B . 2015.07.01
• 3. METHOD FOR DETERMINING TURNING ANGLE OF THRUST VECTOR OF HYPERSONIC ONCE-THROUGH AIR JET ENGINE WITH CHAMFER CUT OF NOZZLE AS PER RESULTS OF FLIGHT TESTS ON HYPERSONIC FLYING LABORATORY [P] . 俄罗斯专利： RU2445599C1 . 2012-03-20

  机译： 超音速飞行实验室飞行试验结果确定带有喷嘴倒角的超音速一次通过式喷气发动机推力矢量转角的方法

• 4. Thrust nozzle for a hypersonic engine [P] . 英国专利： GB2243878A . 1991-11-13

  机译： 高超音速发动机的推力喷嘴

• 5. A THRUST NOZZLE FOR A HYPERSONIC ENGINE [P] . 英国专利： GB9107760D0 . 1991-05-29

  机译： 超音速发动机的推力喷嘴

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• 3. An Experimental Thrust Measurement Study on the Nozzle Asymmetry of Turbulent Pulsed Jets [D] . Leos, Cesar Alberto, Jr. 2020
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• 5. Rocket engine thrust vector control by detonation product injection into the supersonic portion of the nozzle [O] . S.S. Vasyliv, H.O. Strelnykov 2020
• 6. Static Internal Performance of a Single-Engine Onaxisymmetric-Nozzle Vaned-Thrust-Reverser Design with Thrust Modulation Capabilities [R] . Leavitt, L. D., Burley, J. R. 1985

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• 3. Aerodynamic Design of the Bleed Slot in a Hypersonic Quiet Nozzle [J] . Ruiqu Li ,Junmou Shen ,Feng Ji . 应用数学与应用物理（英文） . 2014,第6期
• 4. Overview of Physical and Chemical, Operational Properties of Nitrous Oxide Used as a Propellant for Low-thrust Rocket Engines [J] . A.A.Boryaev . 火炸药学报 . 2019,第1期
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