Intelligent Fault Diagnosis of Liquid Rocket Engine via Interpretable LSTM with Multisensory Data. [PDF]
Sensors (Basel), 2023 Zhang X, Hua X, Zhu J, Ma M.
europepmc +1 more source
Comparison of Rocket Performance using Exhaust Diffuser and Conventional Techniques for Altitude Simulation [PDF]
A rocket engine with an exhaust-nozzle area ratio of 25 was operated at a constant chamber pressure of 600 pounds per square inch absolute over a range of oxidant-fuel ratios at an altitude pressure corresponding to approximately 47,000 feet.
Peters, Daniel J., Sivo, Joseph N.
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Supercharged topping rocket propellant feed system [PDF]
, 1979 A rocket propellant feed system utilizing a bleed turbopump to supercharge a topping turbopump is presented. The bleed turbopump is of a low pressure type to meet the cavitation requirements imposed by the propellant storage tanks.
Ginsburg, A. +2 more
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MODELLING THERMAL BARRIER COATINGS AND THEIR INFLUENCE ON THE LIFETIME OF ROCKET ENGINE NOZZLE STRUCTURES [PDF]
, 2016 Marek Fassin +2 more
openalex +1 more source
Injector-valve device Patent [PDF]
, 1965 Apparatus for cooling and injecting hypergolic propellants into combustion chamber of small rocket ...
Stein, S.
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Experimental validation of rotating detonation for rocket propulsion. [PDF]
Sci Rep, 2023 Bennewitz JW +14 more
europepmc +1 more source
Supersonic-combustion rocket [PDF]
, 1973 A supersonic combustion rocket is provided in which a small rocket motor is substituted for heavy turbo pumps in a conventional rocket engine. The substitution results in a substantial reduction in rocket engine weight. The flame emanating from the small
Franciscus, L. C., Weber, R. J.
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Ablation Characteristics Research in Solid Rocket Motor's Combustion Chamber Produced by 3D Printing. [PDF]
Materials (Basel), 2023 Hui W, Hu Y, Liu Y, Cai Q, Zhao W.
europepmc +1 more source
Electrothermal rockets having improved heat exchangers Patent [PDF]
, 1965 High resistance cross flow heat exchangers for electrothermal rocket ...
Brinich, P. F., Jack, J. R.
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Exploiting technological synergies for future launch vehicles [PDF]
, 2013 Two launch vehicle concepts based on technologies available today or in a short term future in Western Europe are presented. The design of both launchers has the goal of exploiting synergies with current European programs to limit development and ...
Burkhardt, Holger +5 more
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