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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Combustion and Propulsion Research [PDF]
, 1963 Combustion chemistry is one of the oldest branches of chemical science. Among its pioneers must be counted Lavoisier, Bunsen, and others whose names belong among those of the founders of chemical science.
Penner, S. S.
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Ascent trajectory optimisation for a single-stage-to-orbit vehicle with hybrid propulsion [PDF]
, 2012 This paper addresses the design of ascent trajectories for a hybrid-engine, high performance, unmanned, single-stage-to-orbit vehicle for payload deployment into low Earth orbit. A hybrid optimisation technique that couples a population-based, stochastic
Brown, Richard +4 more
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Experimental Research of Supersonic Flow Around Simulating Rocket-Ramjet
MATEC Web of Conferences, 2015 The results of experimental researches of the structure and of the basic parameters of the air when flow around flat and axisymmetric models of rocket-ramjet engine are presented.
Maslov Eugene A. +2 more
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The design and performance estimates for the propulsion module for the booster of a TSTO vehicle [PDF]
A NASA study of the propulsion systems for possible low-risk replacements for the Space Shuttle is presented. Results of preliminary studies to define the USAF two-stage-to-orbit (TSTO) concept to deliver 10,000 pounds to low polar orbit are described ...
Maldonado, Jaime J. +1 more
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COMPUTATIONAL ANALYSIS OF THE MIXING ZONE IN THE COMBUSTION CHAMBER OF RAMJET
Iraqi Journal of Chemical and Petroleum Engineering, 2008 A theoretical analysis of mixing in the secondary combustion chamber of ramjet is presented. Theoretical investigations were initiated to insight into the flow field of the mixing zone of the ramjet combustor and a computer program to calculate ...
Adil A. Al-Hemiri, Sa’ad A. Fa’ek
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Air intakes for a probative missile of rocket ramjet [PDF]
The methods employed to test air intakes for a supersonic guided ramjet powered missile being tested by ONERA are described. Both flight tests and wind tunnel tests were performed on instrumented rockets to verify the designs.
Laruelle, G.
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Study of heat transfer processes in the flowing part of hypersonic air-ramjet engine
MATEC Web of Conferences, 2018 The technique and results of the experimental-theoretical study of gas dynamics, heat transfer and the structure of gas flow in the flowing channel of a model hypersonic air-ramjet engine are presented for Mach numbers M = (5; 6).
Maslov Eugene +4 more
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Hyplane: a single-stage suborbital aerospaceplane. [PDF]
CEAS Space J, 2023 Russo G, Voto C.
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An evaluation of composite propulsion for single-stage-to-orbit vehicles designed for horizontal take-off [PDF]
Composite propulsion was analyzed for single-stage-to-orbit vehicles designed for horizontal take-off. Trajectory, geometric, and mass analyses were performed to establish the orbital payload capability of six engines.
Martin, J. A.
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