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Showing 1 to 19 of 19 for “"Solid propellants"”.

  1. Thermomechanical Meso-Scale Modeling of Combustion of Heterogeneous Solid Propellants

    In the final part of this dissertation, the coupled thermomechanical and propellant surface regression solver is further enhanced through addition of fluid-phase equations for transport of chemical species and temperature. A simple three-step kinetics model is used to describe the complex reactions …

    uiuc Repository record for Thermomechanical Meso-Scale Modeling of Combustion of Heterogeneous Solid Propellants (opens in a new tab)

  2. Exploration and Development of Electrically Controllable Gel and Solid Propellants

    Electrically controllable propellants (ECPs) provide a new method to increase the control and functionality of rocket motors in particular solid rockets. Traditional solid rockets do not have the capability to modify the burning rate on demand during operation, which greatly limits operational …

    vt Repository record for Exploration and Development of Electrically Controllable Gel and Solid Propellants (opens in a new tab)

  3. Measurement and Modeling of Pressure -Driven Transient Burning of Solid Propellants

    … models, applicable to fine oxidizer composite propellants, are examined. The ""surface accumulation model"" supposes that components accumulate in a layer at the surface. Each component reaches an equilibrium concentration inversely proportional to its burning rate. The ""double reaction layer …

    uiuc Repository record for Measurement and Modeling of Pressure -Driven Transient Burning of Solid Propellants (opens in a new tab)

  4. Comparison of Cation-Anion Oxidizer Pairings in Electrically Controllable Solid Propellants

    Electrically controllable solid propellants are an area of interest as a viable solution to the lack of throttle-ability in solid propellant rocket motors. Existing studies have focused on propellants compositions using hydroxyl-ammonium nitrate, ammonium nitrate, or lithium perchlorate as …

    vt Repository record for Comparison of Cation-Anion Oxidizer Pairings in Electrically Controllable Solid Propellants (opens in a new tab)

  5. Methods and analyses for evaluation of erosive burning in solid propellants

    … models for erosive burning in composite propellants were reviewed. The experimental techniques which were cited in the literature for the measurement of erosive burning were also reviewed. Only the high-speed motion picture technique was found to have resolution sufficiently high to …

    vt Repository record for Methods and analyses for evaluation of erosive burning in solid propellants (opens in a new tab)

  6. Modifying burning rate and agglomeration size in aluminized composite solid propellants using mechanically activated metals

    … reduction techniques are important field in solid propellant industry, Large agglomeration results in excessive two phase losses. Tailored composite particles has been applied to tailor aluminum particle ignition and combustion. In this research, mechanical activated aluminum magnesium …

    purdue-thes Repository record for Modifying burning rate and agglomeration size in aluminized composite solid propellants using mechanically activated metals (opens in a new tab)

  7. Theoretical Studies in Two-Phase Flow Prior to the Transition to Detonation in Granular Solid Propellants

    … describing reactive two-phase flow through a gas-solid mixture is presented based upon either the concept of continuum mixture or the concept of separated-flow continuum. The resulting governing equations are solved by the method of finite differences. Details of two distinct numerical methods to …

    uiuc Repository record for Theoretical Studies in Two-Phase Flow Prior to the Transition to Detonation in Granular Solid Propellants (opens in a new tab)

  8. Data Reduction Procedure for an Experimental Method of Measuring the Velocity-Coupled Response Function of Solid Propellants

    … of the velocity-coupled response function of solid-propellants from experimentally measured pressure data. The proposed velocity-coupled response function measurement apparatus consists of an end-burner combustor where the propellant sample is oscillated in a direction normal to the flow in …

    embry-riddle Repository record for Data Reduction Procedure for an Experimental Method of Measuring the Velocity-Coupled Response Function of Solid Propellants (opens in a new tab)

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

    … 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 current study details …

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  10. Development of low-thrust solid rocket motors for small, fast aircraft propulsion

    … current UAV propulsion technologies do not meet. Solid propellant rocket motors could be used, but must be re-engineered to operate at much lower thrust and for much longer burn times than conventional small solid rocket motors. This imposes unique demands on the motor and propellant. This work …

    mit Repository record for Development of low-thrust solid rocket motors for small, fast aircraft propulsion (opens in a new tab)

  11. Combustion signatures of various energetic metal powders in a shock tube experiment

    Metal additives are used in explosives and solid propellants in order to increase the energetic output and effectiveness of the explosives or fuel. Aluminum has been the primary solid fuel additive to solid fuel to improve the combustive properties of propellants. Several other metals are being …

    uiuc Repository record for Combustion signatures of various energetic metal powders in a shock tube experiment (opens in a new tab)

  12. Development, modeling and testing of a slow-burning solid rocket propulsion system

    … do not meet. To meet this need, a slow-burning solid rocket motor has been developed. Such motors require slow-burning solid propellants with tailorable burn rate. This thesis reports experimental results and combustion theory for a slow-burning solid propellant. It also describes a rocket motor …

    mit Repository record for Development, modeling and testing of a slow-burning solid rocket propulsion system (opens in a new tab)

  13. Characterization of a green electric solid propellant for electric propulsion

    <p>"Electric solid propellants are advanced solid chemical rocket propellants that can be controlled (ignited, throttled and extinguished) through the application and removal of an electric current. These propellants are also being considered for use in ablative pulsed plasma thruster and multimode …

    must-thes Repository record for Characterization of a green electric solid propellant for electric propulsion (opens in a new tab)

  14. Examination of the small scale slow cookoff behavior of a cast modified double base propellant

    … measurements of thermally stimulated propellants can be used to improve predictive modelling and safe handling and storage procedures. The primary decomposition products of CMDB were examined using mass spectrometry for stable gas phase species and broadband absorption spectroscopy for …

    uiuc Repository record for Examination of the small scale slow cookoff behavior of a cast modified double base propellant (opens in a new tab)

  15. Microwave enhancement of energetic materials combustion through gas-phase flame interactions

    … to all types of energetic materials, including propellants and pyrotechnics. Thus, a new robust method is needed to control energetic materials' energy release. This work explores microwave interactions with energetic material multiphase flames through interaction with the gas-phase of an …

    iastate Repository record for Microwave enhancement of energetic materials combustion through gas-phase flame interactions (opens in a new tab)

  16. Towards Electrical Control Over Rocket Propellant Combustion

    … performance of various propulsion systems. In solid rocket motors, active burn rate modulation has the potential to enable throttling. In spacecraft propulsion systems, electrolysis of propellants may provide a means to reduce energy requirements and eliminate the need for expensive catalysts. …

    vt Repository record for Towards Electrical Control Over Rocket Propellant Combustion (opens in a new tab)

  17. Investigation of Fuel Geometry and Solid Fuel Combustion for Solid Fuel Ramjets

    Solid fuel ramjets (SFRJs) are a simple means of sustaining supersonic flight. The utilization of solid fuels eliminates the need for moving parts or liquid delivery systems, and the solid fuels are typically inert, resulting in minimal handling requirements compared to solid propellants. …

    vt Repository record for Investigation of Fuel Geometry and Solid Fuel Combustion for Solid Fuel Ramjets (opens in a new tab)

  18. Particle packings and microstructure modeling of energetic materials

    This dissertation explores the use of packings of frictionless hard particles as models of the microstructure of particulate heterogeneous materials. In the first part of this dissertation, we present the current mathematical framework used for understanding the properties of particle packings, as …

    uiuc Repository record for Particle packings and microstructure modeling of energetic materials (opens in a new tab)