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    Space shuttle SRM plume expansion sensitivity analysis. [flow characteristics of exhaust gases from solid propellant rocket engines
    S. D. SmithJ. A. TevepaughM. M. Penny
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    Keywords:
    Solid-fuel rocket
    Rocket engine
    Rocket (weapon)
    Space launch
    Topics:
    Rocket and propulsion systems research
    Energetic Materials and Combustion
    Spacecraft and Cryogenic Technologies
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    G. M. H. J. L. GadiotAlon Gany
    Citations (1)
    Analysis of liquid rocket propellant engine exhaust plumes
    30th Thermophysics Conference (1970)
    T. F. GreenwoodR. J. ProzanA. W. RatliffDave Seymour
    Liquid rocket propellant engine exhaust plume flow field, discussing mathematical models for combustion chamber, throat region and nozzle
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    Arcjet rocket
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    A new technique for simulating rocket engine flow for study of base heating problems
    Howard B. Wilson
    Short duration technique providing simulation of thermodynamic properties and composition of exhaust products of liquid and solid propellant rocket engines
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    A comparison of experimental heat transfer coefficients in a nozzle with analytical predictions from Bartz's methods for various combustion chamber pressures in a solid propellant rocket motor
    D. M. Smith
    Comparison of experimental heat transfer coefficients in a nozzle with analytical predictions for various combustion chamber pressures in solid rocket propellant engine
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    Citations (1)
    Radiation heat transfer in a supersonic nozzle of a solid-propellant rocket engine
    Leonid A. Dombrovsky
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    Thermochemical ablation of materials from normal impingement of solid propellant rocket motor exhaust
    29th Aerospace Sciences Meeting (1978)
    Gary MooreLarry W. AndersonC. LEWISAlan Murray
    Solid-fuel rocket
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    Results from short-duration altitude-chamber techniques for simulating rocket base heating problems.
    Journal of Spacecraft and Rockets (1967)
    Howard B. Wilson
    Covers advancements in spacecraft and tactical and strategic missile systems, including subsystem design and application, mission design and analysis, materials and structures, developments in space sciences, space processing and manufacturing, space operations, and applications of space technologies to other fields.
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    space science
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    An exact solution of a simplified two-phase plume model. [for solid propellant rocket
    S.-Y. WangBarney B. Roberts
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    Ignition and combustion of aluminum in small- scale liquid rocket engines
    Journal of Spacecraft and Rockets (1965)
    L. E. DEANR. C. KEITHT. L. SUMNERM. V. TAYLOR
    Covers advancements in spacecraft and tactical and strategic missile systems, including subsystem design and application, mission design and analysis, materials and structures, developments in space sciences, space processing and manufacturing, space operations, and applications of space technologies to other fields.
    Rocket (weapon)
    Space launch
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    One dimensional internal ballistic calculation for spinning solid rocket motor with conocyl grain
    Journal of Propulsion Technology (1994)
    Weihua ZhangTaiyue CaoYincheng Guo
    Solid-fuel rocket
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