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Performance of a Rotating Detonation Rocket Engine with Various Convergent Nozzles and Chamber Lengths

Energies, 2019
A rotating detonation rocket engine (RDRE) with various convergent nozzles and chamber lengths is investigated. Three hundred hot-fire tests are performed using methane and oxygen ranging from equivalence ratio equaling 0.5–2.5 and total propellant flow ...
J. Bennewitz   +5 more
semanticscholar   +1 more source

Experimental Study of a Hypergolically Ignited Liquid Bipropellant Rotating Detonation Rocket Engine

Journal of Propulsion and Power, 2019
A liquid bipropellant rotating detonation rocket engine was successfully test fired. The 6.5-in.-diam engine operates on a mixture of rocket-grade hydrogen peroxide and triglyme.
W. Anderson, S. Heister, C. Hartsfield
semanticscholar   +1 more source

Single-Phase Instability in Non-Premixed Flames Under Liquid Rocket Engine Relevant Conditions

Journal of Propulsion and Power, 2019
Under rocket-relevant conditions, real-gas effects and thermodynamic nonidealities are prominent features of the flow field.
C. Traxinger, J. Zips, M. Pfitzner
semanticscholar   +1 more source

Rocket Engine with Continuously Rotating Liquid-Film Detonation

Advances in Pulsed and Continuous Detonation, 2018
The possibility of organizing a continuous-detonation combustion of a liquid fuel film in an annular combustor of a detonation liquid-propellant rocket engine has been demonstrated.
S. Frolov   +6 more
semanticscholar   +1 more source

PHM by Using Multi-Physics System-Level Modeling and Simulation for EMAs of Liquid Rocket Engine

IEEE Aerospace Conference, 2019
The need for condition-based maintenance to improve reusable launch vehicle readiness, reliability and safety, with affordable maintenance cost and quick turnaround time is recognized.
K. Kawatsu
semanticscholar   +1 more source

Atomic hydrogen rocket engine

15th International Electric Propulsion, 1981
A rocket using atomic hydrogen propellant is discussed. An essential feature of the proposed engine is that the atomic hydrogen fuel is used as it is produced, thus eliminating the necessity of storage. The atomic hydrogen flows into a combustion chamber and recombines, producing high velocity molecular hydrogen which flows out an exhaust port ...
K. Flurchick, R. D. Etters
openaire   +2 more sources

Experimental Investigations of Film Cooling in a Conical Nozzle Under Rocket-Engine-Like Flow Conditions

AIAA Journal, 2019
The current work presents an experimental parametric study on tangential, supersonic film cooling in the expansion part of a conical nozzle.
S. Ludescher, H. Olivier
semanticscholar   +1 more source

The Rocket Test Engineer

Journal of Jet Propulsion, 1954
Theoretically only one type exists; however, due to the selective process of dynamic evolution, four types are known to exist at various rocket establishments. The IDEAL type is the rocket test engineer you see in the movies, ads, and press releases. He is usually clad in protective clothing, wears a face shield, and sometimes sports a supersonic dunce
openaire   +2 more sources

Development of Soviet Rocket Engines [PDF]

open access: possibleSoviet Review, 1962
It is not always easy to find the source of even a big river. It is only conditionally that we accept the spring inside a log cabin in a small peat bog near the village of Volgoverkhovye as the source of the mighty Volga. It is perhaps even more difficult to find, back in the depths of the ages, the source of the thought which has today become one of ...
openaire   +1 more source

Advancing Europe’s Hybrid Rocket Engine Technology withParaffin and LOX

, 2019
Hybrid rocket engine technology has been advanced enormously at European universities, research institutions and companies in the last decade. New fuels like paraffin-based mixtures have been developed in order to increase regression rate which enables ...
C. Schmierer   +5 more
semanticscholar   +1 more source

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