In-situ propellant rocket engines for Mars mission ascent vehicle [PDF]
When comtemplating the human exploration of Mars, many scenarios using various propulsion systems have been considered. One propulsion option among them is a vehicle stage with multiple, pump fed rocket engines capable of operating on propellants ...
Roncace, Elizabeth A.
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Transient spray combustion characteristics in a gas-liquid pintle rocket engine under acoustic excitation. [PDF]
Sci RepJin X, Zhu C, Chen D, Zhang Z.
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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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Large liquid rocket engine transient performance simulation system [PDF]
Phase 1 of the Rocket Engine Transient Simulation (ROCETS) program consists of seven technical tasks: architecture; system requirements; component and submodel requirements; submodel implementation; component implementation; submodel testing and ...
Mason, J. R., Southwick, R. D.
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Bio-inspired multi-dimensional deep fusion learning for predicting dynamical aerospace propulsion systems. [PDF]
Commun EngVergnolle MQ, Wu EZY, Sui Y, Wang Q.
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Boundary layer integral matrix procedure: Verification of models [PDF]
The three turbulent models currently available in the JANNAF version of the Aerotherm Boundary Layer Integral Matrix Procedure (BLIMP-J) code were studied.
Bonnett, W. S., Evans, R. M.
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Hot Firing Tests of a Gas Generator for Liquid Rocket Engine using a Turbine Manifold Simulator
, 2015 Byoungjik Lim +3 more
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Global 3D rocket launch and re-entry air pollutant and CO2 emissions at the onset of the megaconstellation era. [PDF]
Sci DataBarker CR, Marais EA, McDowell JC.
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