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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Analysis of carbon nano particle variant as the propellant fuel to increase specific impulses of rockets. [PDF]
F1000Res, 2023 Navalino R, Muda N, Hafizah M, Ruyat Y.
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Estimating CO2 emissions due to present and future suborbital space tourism industry. [PDF]
PLoS OneHuang AM, Xu Y.
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Application of Gaussian SVM Flame Detection Model Based on Color and Gradient Features in Engine Test Plume Images. [PDF]
Sensors (Basel)Yan S, Gao Y, Zhang Z, Li Y.
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Active Precipitation of Radiation Belt Electrons Using Rocket Exhaust Driven Amplification (REDA) of Man-Made Whistlers. [PDF]
J Geophys Res Space Phys, 2022 Bernhardt PA +12 more
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Preliminary design of a hybrid rocket engine
The aerospace industry has experienced significant growth in recent years, leading to increased demand for propulsion systems for launch vehicles aimed at placing satellites into orbit, space tourism, upper stages, lunar and planetary landing modules, among other applications. Alongside this growth, there has been a rising demand for propulsion systems
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Predictive maintenance programs for aircraft engines based on remaining useful life prediction. [PDF]
Sci RepXue F, Jin G, Tan L, Zhang C, Yu Y.
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Hybrid rocket engine on the methane clathrate
Kosmìčna nauka ì tehnologìâ, 2017 A.S. Levenko +3 more
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Metal-organic frameworks as hypergolic additives for hybrid rockets. [PDF]
Chem Sci, 2022 Jobin O +8 more
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Magnetohydrodynamic peristaltic flow of hybrid nanofluid in an asymmetric channel with thermal radiation and shape factors: an application of coolant systems. [PDF]
Discov NanoThirunavukarasan K, Sucharitha G.
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