Design and Optimization of a Hybrid Gas Generator for Hydrogen Peroxide Tank Pressurization
Challenges and Issues of Modern SciencePurpose. This study develops a pressurization system for hydrogen peroxide tanks using a hybrid gas generator powered by liquid oxygen and solid fuel.
Mykhailo Vorobei, Mykola Bondarenko
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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.
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Design issues for lunar in situ aluminum/oxygen propellant rocket engines [PDF]
Design issues for lunar ascent and lunar descent rocket engines fueled by aluminum/oxygen propellant produced in situ at the lunar surface were evaluated.
Meyer, Michael L.
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High performance dash on warning air mobile, missile system [PDF]
An aircraft-missile system which performs a high acceleration takeoff followed by a supersonic dash to a 'safe' distance from the launch site is presented.
Castellano, C. R. +2 more
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The design of a Mars Mission Vehicle that would have to be launched by two very heavy lift launch vehicles is described along with plans for a mission to Mars.
Hornung, R.
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Operationally Efficient Propulsion System Study (OEPSS) data book. Volume 4: OEPSS design concepts [PDF]
This study was initiated to identify operations problems and cost drivers for current propulsion systems and to identify technology and design approaches to increase the operational efficiency and reduce operations costs for future propulsion systems. To
Farhangi, Shahram +2 more
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A dynamic simulation approach to optimize thrust regulation in electric pump-fed rocket engines. [PDF]
Sci RepLi T, He H, Yu N, Sun X, Cai G.
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Effect of Correlation on Multi-Engine Rocket Propulsion Systems [PDF]
A matter of great concern in the design and operation of multi-engine rocket propulsion systems is the effect of the premature shutdown of one engine on the vehicle.
Baker, J. R., Breneman, J. E.
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Nano-Iron as a Catalyst in Isocyanate-Free Rocket Propellants. [PDF]
Polymers (Basel)Chmielarek M +2 more
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Test stand design and analysis for Titan 34D static firing [PDF]
The Test Stand 1C at the Air Force Astronautic Laboratory (AFAL), Edwards AFB, Calif., was originally designed for F-1 liquid propellant engines. The stand was modified to handle a five and one half segment Solid Rocket Motor (SRM) Titan 34D vertical ...
Pazargadi, Shayan
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