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Results for “In-cylinder combustion”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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In-Space Manufacturing of Electronics
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Recent Advances in Space Nuclear Propulsion
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Certification Challenges for Batteries in Electric Aviation
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The Pursuit of In-Space Cryogenic Propellant Storage and Transfer
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Core-Centering of Compound Drops in Capillary Oscillations: Observations on USML-1 Experiments in Space
Using the existing inviscid theories, an attempt is made to explain the centering of the oscillating liquid shell. Experiments on liquid shells and liquid-core compound drops were conducted using acoustic levitation, in a low-gravity environment during a Space Shuttle flight. It was observed that their inner and outer interfaces became concentric when excited into capillary oscillations. Using the existing inviscid theories, and attempt is made to explain the centering of the oscillating liquid shell. It is concluded that viscosity needs to be considered in order to provide a realistic description of the centering process.
Autofrettage Crack Growth in COPV liner Material
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Overview of Radiation Modeling in NASA’s ESM Project
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Evaluating Crystallinity in Thermoplastic Composites
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Modeling of Priming Events Using GFSSP in Liquid Propulsion Systems
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Multiscale Modeling of Fracture Strength in Fibrous Thermal Protection System Materials
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Atomic Scale Modeling of Microstructural Features and Defects in Shape Memory Alloys
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Current & Future Challenges in Ceramics for Thermal Protection Systems (TPS)
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Langley’s Work in Thermoplastic Composites and an Overview of the New Ultralight Advanced Composites (ULTRA-COMP) Project
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Stochastic Reconstruction of Ablating Material Properties for Uncertainty Propagation in Material Response Simulations
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3D Reinforced Composites for Improved Impact Resistance in Spacesuits
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Biosynthesized Thermoplastic/Regolith Composites for Closed-Loop In-Space Manufacturing
In-Space Manufacturing (ISM) is vital to supporting a sustained human presence on the Moon or Mars. With payload launch prices ranging from $4,000 to more than $1 million per kg, reducing payload mass is of critical interest. Using in-situ resources for ISM is particularly attractive as it allows for a system of Earth-independent manufacturing for the Lunar surface, reducing the initial payload mass that is required for current ISM systems that rely on terrestrially synthesized materials. This talk presents new composite materials made from Lunar and Martian regolith and Poly(3-hydroxybutyrate) (PHB), a thermoplastic that offers the ability to be biosynthesized in space using various in-situ resources like organic waste or atmospheric CO2 as feedstock. The addition of regolith provides a route to creating materials with a diverse set of properties which will be discussed. The development of these materials represents the first step in creating a system of closed-loop ISM, which is critical to establishing a lasting human presence in space.
Polymer/Regolith Composites for In-Space Manufacturing on the Moon and Mars
In-Space Manufacturing (ISM) is vital to supporting a sustained human presence on the Moon or Mars. With payload launch prices ranging from $4,000 to more than $1 million per kg, reducing payload mass is of critical interest. Using in-situ resources for ISM is particularly attractive as it allows for a system of Earth-independent manufacturing for the Lunar surface, reducing the initial payload mass that is required for current ISM systems that rely on terrestrially synthesized materials. This talk presents new composite materials made from Lunar and Martian regolith and Poly(3-hydroxybutyrate) (PHB), a thermoplastic that offers the ability to be biosynthesized in space using various in-situ resources like organic waste or atmospheric CO2 as feedstock. The addition of regolith provides a route to creating materials with a diverse set of properties which will be discussed. The development of these materials represents the first step in creating a system of closed-loop ISM, which is critical to establishing a lasting human presence in space.