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Showing 1 to 20 of 97 for “"Propulsion and Power"”.

  1. Collimation of deuterium / 3-helium fusion products for advanced spacecraft propulsion and power

    … transpired through the use of chemical rockets, and they have served us well, but they have their limitations. Exploration of the outer solar system, Jupiter and beyond will most likely require a new generation of propulsion system. One potential technology class to provide spacecraft propulsion

    uiuc Repository record for Collimation of deuterium / 3-helium fusion products for advanced spacecraft propulsion and power (opens in a new tab)

  2. Active combustion control : modeling, design and implementation

    Continuous combustion systems common in propulsion and power generation applications are susceptible to thermoacoustic instability, which occurs under lean burn conditions close to the flammability where most emissions and efficiency benefits are achieved, and near stoichiometry where often high …

    mit Repository record for Active combustion control : modeling, design and implementation (opens in a new tab)

  3. THERMAL MANAGEMENT OF ROTATING DETONATION ENGINES

    … to the immense academic progress on the topic and its prospective commercial viability, particularly in relation to aerospace propulsion and power generation systems. One of the major outstanding barriers towards realizing practical RDEs is the issue of intensive heating of the combustor walls. …

    nus Repository record for THERMAL MANAGEMENT OF ROTATING DETONATION ENGINES (opens in a new tab)

  4. Application of a Non-intrusive Optical Non-spherical Particle Sizing Sensor at Turboshaft Engine Inlet

    … environments. Ingesting particulates such as sand or dust can erode and damage engine components. This damage will affect the life cycle of parts and compromise the safety of the aircraft. This issue is very costly and dangerous. In order to combat these issues, a particle sensor with the …

    vt Repository record for Application of a Non-intrusive Optical Non-spherical Particle Sizing Sensor at Turboshaft Engine Inlet (opens in a new tab)

  5. HAPSS, Hybrid Aircraft Propulsion System Synthesis

    <p>Hybrid Aircraft Propulsion System Synthesis (HAPSS) is a computer program that sizes and analyzes pure-series hybrid electric propulsion systems for aircraft. The development of this program began during a NASA SBIR contract, in conjunction with Empirical Systems Aerospace (ESAero), with the …

    calpoly Repository record for HAPSS, Hybrid Aircraft Propulsion System Synthesis (opens in a new tab)

  6. Suppression of premixed combustion dynamics utilizing microjet air injection

    … systems is a major challenge in the field of propulsion and power generation. With the current environmental and political pressure that is being placed on the consumption of fossil fuels, this subject has become even more critical. In the past, the presence of combustion instability could be …

    mit Repository record for Suppression of premixed combustion dynamics utilizing microjet air injection (opens in a new tab)

  7. Investigation of condensed and early stage gas phase hypergolic reactions

    … flown in 1981, feature hydrazine based fuels and nitrogen tetroxide (NTO) based oxidizers. Despite the long history of hypergolic propellant implementation, the processes that govern hypergolic ignition are not well understood. In order to achieve ignition, condensed phase fuel and oxidizer …

    purdue-thes Repository record for Investigation of condensed and early stage gas phase hypergolic reactions (opens in a new tab)

  8. Development of mesoscale burner arrays for next generation compact gas turbines

    … flexibly accommodate a wide range of combustion power outputs. The combustion characteristics of the mesoscale burner array were experimentally investigated using several optical diagnostic and analysis techniques. Lean blow off limit, flame temperature, and NO emission measurements were …

    uiuc Repository record for Development of mesoscale burner arrays for next generation compact gas turbines (opens in a new tab)

  9. Management and control of energy storage systems for stationary and automotive applications

    … 1), reference has been made to some stationary and automotive applications. Stationary applications have regarded Renewable Energy Sources (RESs) exploitation issues and EV integration within micro-grids (Chapter 2). It has been shown that ESSs are particularly useful in compensating for RES …

    cagliari Repository record for Management and control of energy storage systems for stationary and automotive applications (opens in a new tab)

  10. Investigation of Passive Flow Modulation for Full-Scale Air-Oil Coolers for Turbofan Engine Applications

    … aircraft are used every day to transport people and goods around the world. For this reason, a need has been created to improve the thrust specific fuel consumption and improve the fuel efficiency of the engines used for these aircraft. To further improve the efficiency of the turbofan engine …

    embry-riddle Repository record for Investigation of Passive Flow Modulation for Full-Scale Air-Oil Coolers for Turbofan Engine Applications (opens in a new tab)

  11. Development of a High Performance Micropropulsion System for CubeSats

    … defined as satellites with a mass between 0.1 and 1kg (Miniaturized satellite). Picosatellites are typically designed to work together or function in formations (Miniaturized satellite). A specific type of Picosatellite known as CubeSats were introduced in 1999 and since then have increased in …

    calpoly Repository record for Development of a High Performance Micropropulsion System for CubeSats (opens in a new tab)

  12. Comparative simulations of conceptual ion extractors for use in asymmetric inertial electrostatic confinement

    Many deep space propulsion missions currently use ballistic trajectories to reach their destinations. To reduce the times of flight, electric or plasma based propulsion systems are used. While Hall Effect thrusters are the general standard for plasma propulsion, new technologies can enable shorter …

    uiuc Repository record for Comparative simulations of conceptual ion extractors for use in asymmetric inertial electrostatic confinement (opens in a new tab)

  13. Suppression of thermoacoustic instabilities in a swirl combustor through microjet air injection

    … feedback loop coupling heat release rate and acoustic oscillations in a combustor, is one of the greatest challenges currently facing the development of new gas turbine systems for propulsion and power generation. Traditional gas turbine designs have bypassed the problem of combustion …

    mit Repository record for Suppression of thermoacoustic instabilities in a swirl combustor through microjet air injection (opens in a new tab)

  14. The Effect of Thermal Non-Uniformity on Coherent Structures in Supersonic Free Jets

    … noise, with little modification to the engine and nozzle. Prior work has shown that total temperature non-uniformity is a noise reduction technique which introduces a stream of cold flow into the heated jet. This method has been shown to cause changes in the exhaust plume and result in a 2±0.5 …

    vt Repository record for The Effect of Thermal Non-Uniformity on Coherent Structures in Supersonic Free Jets (opens in a new tab)

  15. Prediction of Noise Associated with an Isolated UAV Propeller

    … generation mechanism of a propeller as a mode of propulsion of the said aerial vehicles. Numerical simulation utilizing a Hybrid Large-Eddy Simulation (LES) coupled with Unsteady Reynolds-Averaged Navier-Stokes (RANS) solver, is adopted on an isolated propeller modeled from the commercial DJI …

    embry-riddle Repository record for Prediction of Noise Associated with an Isolated UAV Propeller (opens in a new tab)

  16. Unsteady Internal Ballistics of a Hybrid Rocket

    … simplicity, low cost, operational flexibility, and safety. The flow in the ports of a hybrid rocket motor involves several coupled unsteady phenomena like moving walls, combustion in a boundary layer flow and mass addition along the port, through the regression of the solid fuel wall. The flow …

    embry-riddle Repository record for Unsteady Internal Ballistics of a Hybrid Rocket (opens in a new tab)

  17. Optimal Battery Weight Fraction for Serial Hybrid Propulsion System in Aircraft Design

    <p>This thesis focuses on electric propulsion technology associated with serial hybrid power plants most commonly associated with urban air mobility vehicles. While closed form analytical solutions for parallel hybrid aviation cases have been determined, optimized serial hybrid power plants have …

    embry-riddle Repository record for Optimal Battery Weight Fraction for Serial Hybrid Propulsion System in Aircraft Design (opens in a new tab)

  18. Method and Simulation of On-Orbit Sub-microthrust Evaluation

    … μN precision attitude control for interferometry and imaging missions, finer micro- to sub-micro- thrusters have become an area of high interest. As thrusters are developed and ground-tested, it is necessary to evaluate their thrust performance on-orbit. On-orbit measurements offer actual thrust …

    calpoly Repository record for Method and Simulation of On-Orbit Sub-microthrust Evaluation (opens in a new tab)

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