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Showing 1 to 8 of 8 for “"rocket combustion"”.

  1. Structural analysis of the MIT Micro Rocket Combustion Chamber

    The micro rocket is one of several power microelectromechanical systems (MEMS) under development at MIT. The micro rocket is experiencing structural failures at operating parameters far below the designed performance level. The deterministic strength of brittle materials, such as silicon, is …

    mit Repository record for Structural analysis of the MIT Micro Rocket Combustion Chamber (opens in a new tab)

  2. Numerische Simulation des Wärmeübergangs in einer kryogenen Raketenbrennkammer

    … phenomena on the heat load of a hydrogen/oxygen rocket combustion chamber into the adjacent regenerative cooled wall. The heat transfer in turbulent flow is a result of turbulent vortices and the heat conductivity of the fluid. The turbulent effects were represented by the q-omega Low-Reynolds …

    aachen Repository record for Numerische Simulation des Wärmeübergangs in einer kryogenen Raketenbrennkammer (opens in a new tab)

  3. Early Plume Development and NOx Chemistry in LOx/H₂ and LOx/CH₄ Liquid Rocket Engines

    Projected rocket launch demand in the next 10 years predicts an order-of-magnitude increase in CO₂-equivalent gasses. Despite this expected increase in launch frequency, the on-Earth environmental impacts of off-Earth missions is still understudied, partially due to the lack of combustion and …

    mit Repository record for Early Plume Development and NOx Chemistry in LOx/H₂ and LOx/CH₄ Liquid Rocket Engines (opens in a new tab)

  4. Theoretical And Experimental Investigation Of The Cascading Nature Of Pressure-Swirl Atomization

    … used in IC, aero-engines, and liquid propellant rocket combustion. Understanding the atomization process is important in order to enhance vaporization, mitigate soot formation, design of combustion chambers, and improve overall combustion efficiency. This work utilizes non-invasive techniques …

    ucf

  5. Study of elementary reactions of combustion importance at elevated temperatures and pressures

    … to study the kinetics of elementary reactions of combustion importance at elevated temperatures and pressures. High pressure is encountered in many systems of practical importance such as internal combustion engines and rocket combustion chambers. Several reactions of OH, CH_3 and HO_2 radicals …

    njit Repository record for Study of elementary reactions of combustion importance at elevated temperatures and pressures (opens in a new tab)

  6. Numerical Modeling of a Ducted Rocket Combustor With Experimental Validation

    … a high-fidelity numerical model of a unique combustion flow problem combining multi-phase fuel injection with substantial momentum and temperature into a highly complex turbulent flow. This important problem is very different from typical and more widely known liquid fuel combustion problems …

    vt Repository record for Numerical Modeling of a Ducted Rocket Combustor With Experimental Validation (opens in a new tab)

  7. Design And Implementation Of An Emission Spectroscopy Diagnostic In A High-pressure Strand Burner For The Study Of Solid Propell

    … application of emission spectroscopy to monitor combustion products of solid rocket propellant combustion can potentially yield valuable data about reactions occurring within the volatile environment of a strand burner. This information can be applied in the solid rocket propellant industry. The …

    ucf

  8. Quantitative measurements of temperature using laser-induced thermal grating spectroscopy in reacting and non-reacting flows

    … the spatial distribution of temperature in combustion environments. In addition, the parameters that in influence the local temperature rise due to LITGS were also investigated in continuous vapour flows of acetone/air and toluene/air mixtures at atmospheric conditions. Acetone and toluene …

    cambridge Repository record for Quantitative measurements of temperature using laser-induced thermal grating spectroscopy in reacting and non-reacting flows (opens in a new tab)