Hypersonic cruise aircraft propulsion integration study, volume 1 [PDF]
A hypersonic cruise transport conceptual design is described. The integration of the subsonic, supersonic, and hypersonic propulsion systems with the aerodynamic design of the airframe is emphasized.
Brewer, G. D., Morris, R. E.
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Development of the fuel heating device for the component test of aerospace propulsion systems
Journal of Fluid Science and Technology, 2016 For the next generation space launch vehicle, fully reusable spaceplane with rocket and ramjet combined propulsion system is proposed. That type of spaceplane can drastically reduce the cost per unit mass of the payload.
Mitsuhiro SOEJIMA +3 more
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Hypersonic Airbreathing Missile [PDF]
A hypersonic airbreathing missile using dual mode scramjet engines for propulsion is described. The fuselage is constructed of a material with a high heat sink capacity and is covered with a thermal protective shield and lined with an internal insulating
Hunt, J. L. +2 more
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Thermal design and analysis of a hydrogen-burning wind tunnel model of an airframe-integrated scramjet [PDF]
An aerodynamic model of a hydrogen burning, airframe integrated scramjet engine has been designed, fabricated, and instrumented. This model is to be tested in an electric arc heated wind tunnel at an altitude of 35.39 km (116,094 ft.) but with an inlet ...
Guy, R. W. +3 more
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Langley Mach 4 scramjet test facility [PDF]
An engine test facility was constructed at the NASA Langley Research Center in support of a supersonic combustion ramjet (scramjet) technology development program.
Anderson, G. Y. +4 more
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Airframe-integrated propulsion system for hypersonic cruise vehicles [PDF]
Research on a new, hydrogen burning, airbreathing engine concept which offers good potential for efficient hypersonic cruise vehicles is considered. Features of the engine which lead to good performance include; extensive engine-airframe integration ...
Huber, P. W., Jones, R. A.
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Numerical Study of Transverse Injection into Supersonic flow of the Scramjet Combustor [PDF]
فناوری در مهندسی هوافضا, 2018 Nowadays efforts for development of the scramjet engines are increased. Scramjet engines use atmospheric oxygen as an oxidizer therefore they don’t need oxidizer tanks, thus the weight of these systems is less than comparable rocket systems.
Mostafa Zahedzadeh, Fathollah Ommi
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CFD Investigation of Supersonic Scramjet Exhaust Geometry for Emission Reduction and Sustainable Hypersonic Propulsion [PDF]
EPJ Web of ConferencesThis study employs CFD analysis to optimize the scramjet exhaust divergent angle with the aim of improving propulsion efficiency and reducing environmental impact in hypersonic flight.
Paramadhayalan P. +8 more
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Enhancement of the CAVE computer code [PDF]
The computer code CAVE (Conduction Analysis via Eigenvalues) is a convenient and efficient computer code for predicting two dimensional temperature histories within thermal protection systems for hypersonic vehicles.
Burk, H. O., Rathjen, K. A.
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Expanded operational capabilities of the Langley Mach 7 Scramjet test facility [PDF]
An experimental research program conducted to expand the operational capabilities of the NASA Langley Mach 7 Scramjet Test Facility is described. Previous scramjet testing in this facility was limited to a single simulated flight condition of Mach 6.9 at
Guy, R. W., Thomas, S. R.
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