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Showing 1 to 20 of 53 for “"Thermal Protection"”.

  1. Characterization of carbon ablators for hypersonic thermal protection systems

    … vehicle's kinetic energy is rapidly converted to thermal energy, generating extreme heat and caustic chemical conditions that rapidly destroy even the most advanced materials. Surviving such an environment depends entirely on the thermal protection system (TPS). Ablative materials, which dissipate …

    uiuc Repository record for Characterization of carbon ablators for hypersonic thermal protection systems (opens in a new tab)

  2. Thermal protection concepts for mobile and dusty lunar experiments.

    Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics. Thesis. 1971. M.S.

    mit Repository record for Thermal protection concepts for mobile and dusty lunar experiments. (opens in a new tab)

  3. Modeling the oxidation, ablation, and mechanics of carbon fiber preform in thermal protection systems

    Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2025-10-20 without embargo terms

    uiuc Repository record for Modeling the oxidation, ablation, and mechanics of carbon fiber preform in thermal protection systems (opens in a new tab)

  4. Assessment of damage to thermal protection systems due to micrometeoroid and orbital debris impacts

    Thermal protection systems for hypersonic vehicles are low- to zero-fault-tolerant. In order to understand the fault tolerance of this system, the number of impacts that cause mission failure due to micro-meteoroid and orbital debris damage is presented. This number differs based on the mission, so …

    uiuc Repository record for Assessment of damage to thermal protection systems due to micrometeoroid and orbital debris impacts (opens in a new tab)

  5. Detection of Hydrogen in a Two-Phase Cryogen Flow Stream with Thermal Protection Design Configurations

    <p>All commercial liquid-propelled rockets use hydrogen as means to reach outer space. These rocket boosters are tested on the ground and use hydrogen as means of purging the remaining explosive gasses left in the test tanks. To conserve helium, a non-renewable resource, a test fixture was …

    usm Repository record for Detection of Hydrogen in a Two-Phase Cryogen Flow Stream with Thermal Protection Design Configurations (opens in a new tab)

  6. A Lagrangian, Discontinuous-Galerkin Material Response Solver for the Analysis of Ablative Thermal Protection Systems

    Thermal protection systems (TPS) play a vital role in safeguarding aerospace vehicles from the intense aerodynamic heating encountered during hypersonic flight. One category of TPS materials manages extreme heat through pyrolysis, a process in which the elevated temperatures trigger an endothermic …

    mit Repository record for A Lagrangian, Discontinuous-Galerkin Material Response Solver for the Analysis of Ablative Thermal Protection Systems (opens in a new tab)

  7. Development, modeling and testing of thermal protection systems in small, slow-burning solid rocket motors

    … Such a propulsion system presents unique thermal challenges due to the long exposure times and the close proximity of temperature sensitive vehicle components to the combustion reactions. This thesis presents the development of a thermal management system appropriate for small, slow …

    mit Repository record for Development, modeling and testing of thermal protection systems in small, slow-burning solid rocket motors (opens in a new tab)

  8. An Aero-Thermo-Chemo-Mechanical Coupling Framework for the Analysis of Hypersonic Ablative Thermal Protection Systems

    … modeling of the hypersonic flight of ablative thermal protection systems (TPS): resolving the relevant coupled physical phenomena through multi-physics simulations, the management of the disparate spatiotemporal scales associated with the fluid and solid responses, and establishing a reliable …

    mit Repository record for An Aero-Thermo-Chemo-Mechanical Coupling Framework for the Analysis of Hypersonic Ablative Thermal Protection Systems (opens in a new tab)

  9. An approximate method of calculating the weight of the two- insulation-two-coolant thermal protection system

    … total weight of the two-insulation--two-coolant thermal protection system is developed. The equations derived in the development of the approximate method enable insight into the parameters that control the system weight. Two cases are considered: the case where the outer coolant location is …

    vt Repository record for An approximate method of calculating the weight of the two- insulation-two-coolant thermal protection system (opens in a new tab)

  10. Comprehensive Modeling of Novel Thermal Systems: Investigation of Cascaded Thermoelectrics and Bio-Inspired Thermal Protection Systems Performance

    Thermal systems involve multiple components assembled to store or transfer heat for power, cooling, or insulation purpose, and this research focuses on modeling the performance of two novel thermal systems that are capable of functioning in environments subjected to high heat fluxes. The first …

    vt Repository record for Comprehensive Modeling of Novel Thermal Systems: Investigation of Cascaded Thermoelectrics and Bio-Inspired Thermal Protection Systems Performance (opens in a new tab)

  11. Assessment of the effect of designed-in features on thermal protection systems with application to vascular self-healing

    Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2022-11-11 without embargo terms

    uiuc Repository record for Assessment of the effect of designed-in features on thermal protection systems with application to vascular self-healing (opens in a new tab)

  12. Advancing Autonomous Structural Health Monitoring

    … source. Aerospace vehicles are equipped with thermal protection systems to isolate internal components from harsh reentry conditions. While the thermal protection systems are critical to the safety of the vehicle, finding damage in these structures presents a unique challenge. Impedance …

    vt Repository record for Advancing Autonomous Structural Health Monitoring (opens in a new tab)

  13. Assessment of aerocapture-entry trajectories for human Mars exploration

    … system, a higher entry velocity, and a reusable thermal protection system on aerocapture-entry system mass requirements is explored. Results indicate that the thermal protection system thickness does not vary significantly with parking orbit selection while shorter period orbits require more …

    uiuc Repository record for Assessment of aerocapture-entry trajectories for human Mars exploration (opens in a new tab)

  14. Uncertainty quantification applied to the analysis and design of a hypersonic inflatable aerodynamic decelerator for spacecraft reentry

    … fluid-structure interaction, and flexible thermal protection system response of a deformable inflatable decelerator. Uncertainty analysis is first applied to the hypersonic flowfield simulations to quantify the uncertainty in the surface convective and radiative heat flux, pressure, and …

    must-thes Repository record for Uncertainty quantification applied to the analysis and design of a hypersonic inflatable aerodynamic decelerator for spacecraft reentry (opens in a new tab)

  15. Computation of Hypersonic Flows with Lateral Jets Using k-ω Turbulence Model

    <p>Thermal Protection systems (TPS) are used as shields in space vehicles which encounter high heat and temperatures at the reentry altitudes. Among them, the cooling techniques and the ablative coatings are most popular. However, they have their own weight limitations. In the recent decade, …

    embry-riddle Repository record for Computation of Hypersonic Flows with Lateral Jets Using k-ω Turbulence Model (opens in a new tab)

  16. Scale-bridging molecular dynamics simulations of plasma-surface interactions

    … plasma facing components in reactor vessels and thermal protection system in re-entry spacecraft. Due to the complex chemistry at the plasma surface boundaries, it is difficulty to either control or predict the effect of plasma on the patterning or erosion of the material. In this dissertation, …

    uiuc Repository record for Scale-bridging molecular dynamics simulations of plasma-surface interactions (opens in a new tab)

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

    … their size (and thus have low chamber pressure), thermal protection for the motor case, and small nozzles which can withstand long burn times.

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

  18. Preliminary design of a high enthalpy plasma tunnel for atmospheric re-entry research

    … their interactions with a downstream sample of thermal protection material, and the response of the material as it is exposed to high reactive, high-temperature flow. The data collected from the experiments conducted at the facility will be used to verify computer models as well as material …

    uiuc Repository record for Preliminary design of a high enthalpy plasma tunnel for atmospheric re-entry research (opens in a new tab)

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