Results 181 to 190 of about 10,850 (227)

Propulsion Options for the Hypersonic Research Airplane

Journal of Aircraft, 1975
release. During the analysis of technology capabilities and requirements, it became apparent that capability would not be limited to advanced space Shuttle launch systems, but would also be applicable to supersonic-hy personic military aircraft and advanced hypersonic transport systems.
Verle V. Van Camp, E.T. Williams
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Facility requirements for hypersonic propulsion system testing

27th Aerospace Sciences Meeting, 1989
Facility requirements for hypersonic propulsion system testing and the capabilities or limitations of selected hypersonic testing facilities are briefly reviewed. The specific advantages and limitations of the shock tunnel for hypersonic propl.;1.sion testing are discussed, and areas are identified where shock-tunnel research can supplement other ...
M. DUNN, J. LORDI, C. WITTLIFF, M. HOLDEN   +3 more
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Combined cycle propulsion for hypersonic flight

Acta Astronautica, 1988
Abstract Major advances in air breathing/combined cycle propulsion for hypersonic flight during the past three decades are reviewed. A proliferation of combined cycle concepts were identified and studied in sufficient detail to permit trade-off analyses to be conducted during the 1950's and 1960's.
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Hypersonic airbreathing propulsion

2000
The potential for use of scramjet propulsion systems is discussed. The applications currently under consideration in the USA are long range missiles, hypersonic aircraft, single stage to orbit vehicles and orbital transfer vehicles (OTV). Experimental shock tunnel testing of a scramjet model at the University of Queensland is described, and its ...
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A course in hypersonic propulsion at Purdue University

31st Joint Propulsion Conference and Exhibit, 1995
Early in 1992, the development of a new course, 'Hypersonic Propulsion,' began at Purdue University. The initial offering of this course occurred in the spring semester of 1993, and the course has been offered each spring since. The challenge to develop a meaningful course in a subject area that is still largely in the research stage was considerable ...
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The Scramjet: A Solution for Hypersonic Aerodynamic Propulsion

41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2005
The challenge of achieving hypersonic velocities with an air -breathing engine has been the prospect since the late 1950’s. The space program and the Lunar landings and the introduction of the ballistic missiles seemed however to be the confirmation that the rocket technology was the means to reach high velocities and long ranges.
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Optimisation of Hypersonic Vehicles for Airbreathing Propulsion [PDF]

, 2010
A significant proportion of current and near-term space applications have masses of only a few hundred kilograms. Orbiting those is associated with stringent economical burdens in light of the typically low payload mass fractions (
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Criteria for hypersonic airbreathing propulsion and its experimental verification

Chinese Journal of Aeronautics, 2021
Zonglin Jiang, Zijian Zhang, Yunfeng Liu   +2 more
exaly  

The Rebirth of Round Hypersonic Propulsion

42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2006
Melvin Bulman, Adam Siebenhaar
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Standing oblique detonation for hypersonic propulsion: A review

Progress in Aerospace Sciences, 2023
Zonglin Jiang
exaly