1–20 von 53 Ergebnissen
|

    The ultimate limits of the relativistic rocket equation. The Planck photon rocket

    Haug, Espen Gaarder | Elsevier | 2017
    Schlagwörter: Relativistic rocket equation , Rocket load , Maximum speed rocket

    Comment on “the ultimate limits of the relativistic rocket equation. The Planck photon rocket”

    Tommasini, Daniele / Paredes, Angel / Michinel, Humberto | Elsevier | 2019
    Schlagwörter: Relativistic rocket equation , Rocket load , Maximum speed rocket

    Analytic approach to determine optimal conditions for maximizing altitude of sounding rocket

    Lee, Sang-Hyeon | Elsevier | 2014
    Schlagwörter: Sounding rocket , Rocket momentum equation

    Relativistic rocket and space flight

    Walter, Ulrich | Elsevier | 2006
    Schlagwörter: Relativistic rocket , Rocket equation

    Numerical Simulation of Ionized Rocket Plumes

    Gueyffier, D. / Fromentin-Denoziere, B. / Simon, J. et al. | AIAA | 2014
    Schlagwörter: Solid Rocket Motor , Rocket Performance , Maxwell Equation

    Numerical simulation of the infrared radiative signatures of liquid and solid rocket plumes

    Cai, Guobiao / Zhu, Dingqiang / Zhang, Xiaoying | Elsevier | 2007
    Schlagwörter: Rocket plume , Radiative transport equation

    Computational Fluid Dynamics Simulation of Hybrid Rockets of Different Scales

    Lazzarin, M. / Faenza, M. / Barato, F. et al. | AIAA | 2015
    Schlagwörter: Hybrid Rocket , Rocket Engine Performance , Antoine Equation

    Multiphysics Modeling for Combustion Instability in Paraffin-Fueled Hybrid Rocket Engines

    Casalino, Lorenzo / Ferrero, Andrea / Folcarelli, Lorenzo et al. | AIAA | 2024
    Schlagwörter: Hybrid Rocket Engines , Heat Equation

    An Approximate Calculation for Supersonic Flow past Bodies of Rocket Vehicles. Part I - Linearized Flow with Axial Symmetry

    T. Tani | NTIS | 1965
    Schlagwörter: Rocket vehicle , Wave equation , Equation , Rocket

    Liquid Films Instability Analysis of Liquefying Hybrid Rocket Fuels Under Supercritical Conditions

    Adachi, Masaki / Shimada, Toru | AIAA | 2014
    Schlagwörter: Hybrid Rocket Fuel , Redlich Kwong Equation of State , Hybrid Rocket Engines

    SINGULAR EXTREMALS IN LAWDEN'S PROBLEM OF OPTIMAL ROCKET FLIGHT

    Kelley, H. J. | NTRS | 1963
    Schlagwörter: ROCKET FLIGHT , EULER-LAGRANGE EQUATION

    Research in and Application of Modern Automatic Control Theory to Nuclear Rocket Dynamics and Control Progress Report, Feb. 1 - Sep. 1, 1964

    D. L. Hetrick / J. L. Melsa / H. S. Murray et al. | NTIS | 1965
    Schlagwörter: Nuclear rocket , Equation , Rocket

    On an application of the hamilton-jacobi theory to high thrust rocket flight

    Nafoosi, A. A. / Passmore, H. | NTRS | 1965
    Schlagwörter: ROCKET FLIGHT , HAMILTON-JACOBI EQUATION

    Validation of Transverse Instability Damping Computations for Rocket Engines

    Sattelmayer, Thomas / Kathan, Robert / Köglmeier, Stefan et al. | AIAA | 2015
    Schlagwörter: Rocket Engine , Liquid Rocket Combustion Chambers , Acoustic Wave Equation

    A method for calculating the laser rocket engine thermal state based on the optical discharge with numerous plasma formations

    Sattarov, A. G. | Springer Verlag | 2010
    Schlagwörter: laser rocket engine , criterional equation

    A general method for determining optimum thrust nozzle contours for gas-particle flows.

    Hoffman, J. D. / Thompson, H. D. | NTRS | 1966
    Schlagwörter: ROCKET NOZZLE , DIFFERENTIAL EQUATION

    Algebraic Approach to the Minimum-Cost Multi-Impulse Orbit-Transfer Problem

    Avendaño, M. / Martín-Molina, V. / Martín-Morales, J. et al. | AIAA | 2016
    Schlagwörter: Tsiolkovsky Rocket Equation

    Small Satellite Rendezvous Using Differential Lift and Drag

    Horsley, M. / Nikolaev, S. / Pertica, A. | AIAA | 2013
    Schlagwörter: Rocket Engine , Clohessy Wiltshire Equation

    Rankine Vortex Formation in Cylindrical Tanks with Curved Base: An Experimental Investigation

    Harish, Sankar / Hariharan, S. K. / Shajahan, Ashiq et al. | AIAA | 2022
    Schlagwörter: Bernoulli's Equation , Liquid Propellant Rocket Engine

    Improved Linearized Breakup Model for the Liquid Sheets Produced by Swirl Atomizers

    Arun Vijay, G. / Shenbaga Vinayaga Moorthi, N. | AIAA | 2015
    Schlagwörter: Liquid Fuel Rocket , Continuity Equation