Analysis of the kerosene combustion simulation for a liquid-propellant rocket engine [PDF]
, 2022 Maxim Nikolaevich Senchev +3 more
openalex +1 more source
The effect of plasmoid drifts on the pellet rocket effect in magnetic confinement fusion plasmas [PDF]
arXivWe detail here a semi-analytical model for the pellet rocket effect, which describes the acceleration of pellets in a fusion plasma due to asymmetries in the heat flux reaching the pellet surface and the corresponding ablation rate. This effect was shown in experiments to significantly modify the pellet trajectory, and projections for reactor scale ...
arxiv
Low viscosity magnetic fluid obtained by the colloidal suspension of magnetic particles Patent [PDF]
, 1965 Low density and low viscosity magnetic propellant for use under zero gravity ...
Papell, S. S.
core +1 more source
Dual-fuel, dual-mode rocket engine [PDF]
, 1989 The invention relates to a dual fuel, dual mode rocket engine designed to improve the performance of earth-to-orbit vehicles. For any vehicle that operates from the earth's surface to earth orbit, it is advantageous to use two different fuels during its ...
Martin, James A.
core +1 more source
Combustor design and analysis using the Rocket Combustor Interactive Design (ROCCID) methodology [PDF]
The ROCket Combustor Interactive Design (ROCCID) Methodology is a newly developed, interactive computer code for the design and analysis of a liquid propellant rocket combustion chamber.
Klem, Mark D. +2 more
core +1 more source
Journal of Aerospace Technology and Management, 2011 The main objective of this work was to present the specifi cation of an experimental fi ring test stand for liquid rocket engines (LRE) and develop a program for control and acquisition of data.
Emerson Andrade Santos +3 more
doaj
Optimal Selection of Fuel Bias and Propellant Residual Analysis of a Liquid Rocket
, 2015 Eun-Jung Song +2 more
openalex +2 more sources
Verification of a hydrodynamic model of a liquid-propellant rocket engine’s cavitating pumps using experimental and theoretical pump transfer matrices [PDF]
, 2020 S.I. Dolgopolov
openalex +1 more source
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.
europepmc +1 more source