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Launching Process for Variable-Mass Rockets by Series Solution
Journal of Mechanical Engineering and Technology, 2013In this study, the mathematical investigation of rocket motion path is presented using analytical and numerical methods . Differential transform method and fourth-order Runge-Kutta method are used for solving the current problem. A parametric study is performed which includes the effect of exhaust velocity (Ce), burn rate (BR) of fuel and diameter of ...
M. Gorji +4 more
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Acta Mechanica, 2020
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This paper presents a hybrid analytical framework for modeling the two-dimensional motion of a rocket with variable mass, incorporating mass loss due to fuel expenditure. While classical approaches like Tsiolkovsky’s rocket equation focus on one-dimensional motion, real-world launch vehicles experience complex 2D trajectories influenced by thrust ...
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Experimental investigation of erosion rate of insulation materials using hybrid rockets
FirePhysChem, 2021Pa Ramakrishna
exaly
Derivation of Motion Equation of Variable Mass Moving Rocket
Applied Physics, 2018openaire +1 more source
FREE VIBRATION CHARACTERISTICS OF VARIABLE MASS ROCKETS HAVING LARGE AXIAL THRUST/ACCELERATION
Journal of Sound and Vibration, 1995openaire +1 more source
Performance of Mixture-Ratio-Controlled Hybrid Rockets Under Uncertainties in Fuel Regression
Journal of Propulsion and Power, 2021Toru Shimada
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Challenges of Ablatively Cooled Hybrid Rockets for Satellites or Upper Stages
Aerospace, 2021Francesco Barato
exaly