Synonyme wurden verwendet für: Propellant mass ratio
Suche ohne Synonyme: keywords:(Propellant mass ratio)

1–20 von 69 Ergebnissen
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    Performance of Mixture-Ratio-Controlled Hybrid Rockets for Nominal Fuel Regression

    Ozawa, Kohei / Shimada, Toru | AIAA | 2020
    Schlagwörter: Propellant Mass Ratio , Mass Flow Rate , Aspect Ratio

    Novel Testing of a Water-Breathing Naval Ramjet at Underwater Cruise Conditions

    Eisen, Nachum E. / Gany, Alon | AIAA | 2022
    Schlagwörter: Propellant Mass Ratio

    SLS Dual Use Upper Stage (DUUS) Opportunities

    S. Creech / J. Holladay / D. Jones | NTIS | 2013
    Schlagwörter: Propellant mass ratio

    Saturn s-iv cryogenic weigh system. i - propellant utilization.

    Hendee, E. A. / Nichols, R. H. | NTRS | 1965
    Schlagwörter: CRYOGENIC PROPELLANT , PROPELLANT MASS RATIO

    Nondeterministic Analysis of Monopropellant Catalyst Bed Model

    Kerr, Daniel H. / Karagozian, Ann R. / Bilyeu, David et al. | AIAA | 2020
    Schlagwörter: Propellant Mass Fraction , Aspect Ratio , Mass Flow Rate

    Performance Comparison Between a Magnesium- and Xenon-Fueled 2 Kilowatt Hall Thruster

    Hopkins, Mark A. / King, Lyon B. | AIAA | 2016
    Schlagwörter: Bismuth Propellant , Thrust to Power Ratio , Magnesium Propellant , Mass Flow Rate

    Coaxial Jet Flame Subject to Long-Wavelength Acoustic Oscillations

    Sirignano, William A. / Krieg, Jeremy | AIAA | 2016
    Schlagwörter: Liquid Propellant Rocket Engine , Temperature Ratio , Total Mass Flow Rate , Propellant

    Methodology for Geometric Optimization and Sizing for Subnewton Monopropellant Catalyst Beds

    Fonda-Marsland, Ewan / Roberts, Graham T. / Ryan, Charles N. et al. | AIAA | 2021
    Schlagwörter: Propellant , Aspect Ratio , Mass Flow Rate

    In Situ Propellant Alternatives for a Lunar Ascent/Descent Vehicle

    Nikitaeva, Daria / Dale Thomas, L. | AIAA | 2023
    Schlagwörter: Propellant Mass Fraction , Thrust to Weight Ratio , Liquid Oxygen Propellant

    Swirl Injection of Gaseous Oxygen in a Lab-Scale Paraffin Hybrid Rocket Motor

    Quadros, Flávio D. A. / Lacava, Pedro T. | AIAA | 2019
    Schlagwörter: Mass Flow Rate , Propellant , Aspect Ratio

    Efficiency Mechanisms in Porous-Media Electrospray Thrusters

    Natisin, Michael R. / Zamora, Henry L. / Holley, Zachary A. et al. | AIAA | 2021
    Schlagwörter: Total Mass Flow Rate , Propellant , Thrust to Power Ratio

    Investigation of a Ducted Rocket with a Paraffin/Oxygen Hybrid Gas Generator

    Komornik, Daniel / Gany, Alon | AIAA | 2019
    Schlagwörter: Mass Flow Rate , Propellant Burn Rate , Fuel Air Ratio

    Dependence of Pellet Shape and Size on Pressure Drop in H 2 O 2 Thrusters

    Koopmans, R.-J. / Shrimpton, J. S. / Roberts, G. T. et al. | AIAA | 2014
    Schlagwörter: Mass Flow Rate , Green Propellant , Aspect Ratio

    Improving the Hall Thruster Global Efficiency over a Wide Flow-Rate Range

    Fan, Hao-tian / Li, Hong / Mao, Wei et al. | AIAA | 2021
    Schlagwörter: Propellant , Mass Flow Rate , Thrust to Weight Ratio

    Spacedrives and Conservation Laws

    Sedwick, Raymond / White, Harold | AIAA | 2018
    Schlagwörter: Propellant , Mass Flow Rate , Thrust to Power Ratio

    Rocket Equation with Burn Losses and Propellant Tanks Jettison

    Teixeira, Filipe A. C. G. / Gil, Paulo J. S. | AIAA | 2021
    Schlagwörter: Propellant , Thrust to Weight Ratio , Mass Flow Rate

    Modeling of Pogo Vibration in Rockets with Staged Combustion Cycle Engine

    Wang, Zhao / Shujun, Tan / Jinfan, Liu et al. | AIAA | 2021
    Schlagwörter: Liquid Propellant Rocket , Mass Flow , Critical Damping Ratio

    Microfabricated Electrospray Thruster Array with High Hydraulic Resistance Channels

    Grustan-Gutierrez, Enric / Gamero-Castaño, Manuel | AIAA | 2017
    Schlagwörter: Propellant , Mass Flow Rate , Aspect Ratio

    Feasibility and Performance of Atmospheric-Breathing Propulsion for Mars Descent

    Gonyea, Keir C. / Braun, Robert D. / Auslender, Aaron H. | AIAA | 2017
    Schlagwörter: Propellant Mass Fraction , Thrust to Weight Ratio

    Criteria for optimum propellant mixing in impinging-jet injection elements.

    Riebling, R. W. | NTRS | 1967
    Schlagwörter: PROPELLANT MASS RATIO