Software

Design Environment for Multi-Fidelity and Multi-Disciplinary Components

John H. Glenn Research Center, Cleveland, Ohio Many of the most challenging aspects of propulsion system development are related to the prediction of interacting effects among fluid loads, thermal loads, and structural deflection. A typical design practice might ignore the interaction between the physical phenomena where the outcome of each analysis can be heavily dependent on the inputs. Such a rigid design process also lacks the flexibility to employ multiple levels of fidelity in the analysis of each of the components.

Posted in: Mechanical Components, Software, Briefs

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Shipping Foam Designer Software

Lyndon B. Johnson Space Center, Houston, Texas An easy-to-use design tool was developed in response to a large number of documented cases of critical (flight and ground) hardware failing after experiencing drops during commercial shipment. By entering the mass of the hardware to be protected, and the drop height, the software helps the user select the type and dimensions of the shock attenuating foam needed. Hundreds of drop tests were conducted with metal plates instrumented with accelerometers that were protected by common shipping foams of different thicknesses, along with foam compression tests conducted at various speeds to develop mathematical material models for these foams. The foam drops were video recorded at a very high rate of speed to capture foam deformation due to drop.

Posted in: Mechanical Components, Software, Briefs

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Evolutionary Mission Trajectory Generator

Goddard Space Flight Center, Greenbelt, Maryland The Evolutionary Mission Trajectory Generator (EMTG) is a global trajectory optimization tool for designing interplanetary missions that perform multiple flybys and either low-thrust or high-thrust propulsive maneuvers on the way to destinations in the solar system. Some targets, such as Mars and Venus, are reachable using direct flights with chemical propulsion technology. Others, such as Mercury, main-belt asteroids, and comets are not easily accessible. One way to mitigate this problem is by using more efficient propulsion systems, such as low-thrust solar electric propulsion. Another is to find more efficient paths to the destination, possibly including gravity assist maneuvers, or planetary flybys.

Posted in: Mechanical Components, Software, Briefs

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Visual International Space Station Configuration Viewing Tool

Lyndon B. Johnson Space Center, Houston, Texas Communicating the current International Space Station (ISS) configuration and also potential ISS configurations is a necessity during ISS trade studies and Ops Con development. Often, multiple configuration options will need to be communicated. Doing so without a means of displaying an image of the description can be very confusing. Historically, visual information needed for presentations and meetings was conveyed using still images or pre-generated videos. This form of information provides only a single view, and it is not always at the optimum location.

Posted in: Mechanical Components, Software, Briefs

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Two-Equation Turbulence Models for Application to Internal Flow Through Pneumatic Valves

Applications include design, analysis, and optimization of valves and pumps. John F. Kennedy Space Center, Florida Predicting turbulent flowfield and pressure drop in complex internal flows, such as valves, pumps, and turbines, is of great interest in many areas of technology. Accurate prediction of three-dimensional (3D) flowfield in complex devices is critically dependent on the accuracy of the turbulence model used to describe the turbulence energy production and dissipation processes within the flowfield region of interest.

Posted in: Mechanical Components, Software, Briefs

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Multi-Species Turbulent Mixing Under Supercritical-Pressure Conditions

This mixing model under high-pressure conditions would be useful for automotive, gas turbine engine, and liquid rocket engine companies. NASA’s Jet Propulsion Laboratory, Pasadena, California A model describing supercritical-pressure, multi-species turbulent mixing has been developed to simulate situations prevailing in diesel, gas turbine, and HCCI (homogeneous charge compression ignition) engines. It is also a situation occurring in atmospheric planetary science, such as the Venus atmosphere. Previously, there had been no model to describe this high-pressure mixing under turbulent conditions.

Posted in: Materials, Software, Briefs

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A Model of Reduced Oxidation Kinetics Using Constituents and Species

The advantage of such a simple model becomes increasingly significant with increasing carbon atoms of the fuel. NASA’s Jet Propulsion Laboratory, Pasadena, California Elementary-reaction chemical kinetics of hydrocarbon oxidation consists of hundreds to thousands of species and thousands of reactions. As such, it is impossible to use it in models and codes involving turbulence because computations are unfeasible due to lack of memory and computer speed. The solution is to reduce the elementary chemical kinetics to a much smaller set of representative reactions. A kinetic reduction has been shown to work very well for isooctane and its mixtures with n-pentane, iso-hexane, and n-heptane.

Posted in: Materials, Software, Briefs

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