NASA_Software_Catalog_2014.pdf#sthash.Rk7M8wlL

Charring Material Ablator (CMA87) CodeMFS-32299-1The Charring Material Ablator (CMA87) code is a predictive software program that performs thermal andablative analysis of rocket nozzle liner materials. The software is written in ANSI-standard Fortran 77 and usesstandard mathematical functions found in common linkable object libraries on most high-end workstationsand/or PC platforms.U.S. Release OnlyCMA92FLO Aerotherm Charring Material Thermal Response Ablating ProgramMFS-31355-1The CMA92FLO Aerotherm Charring Material Thermal Response Ablating Program is an implicit finitedifferencecomputational procedure.U.S. Release OnlyCMA93FLO Aerotherm Charring Material Thermal Response Ablating ProgramMFS-31767-1In this version of the Aerotherm Charring Material Thermal Response Ablating Program, developed for NASAby Aerotherm, a line of code was altered so the program would read input data from a previous file ratherthan waiting for operator input from an interactive terminal.U.S. Release OnlyCollaborative Spacecraft and Mission Software Design Tool (ATLAS)ARC-16674-1ATLAS is a software tool used to do preliminary design studies for spacecraft missions. The software supportsa collaborative work environment allowing multiple engineers to work simultaneously on the same design.U.S. and Foreign Release (Academic)Computational Fluid Dynamics (CFD) Utility Software LibraryARC-14467-1AA collection of utility programs and reusable subroutine libraries supports computational fluid dynamics,particularly on multiblock structured grids. The technology is applicable to all flight regimes—subsonic,transonic, supersonic, and hypersonic. The CFD Utility Software Library can be downloaded at:Open SourceComputational Fluids Laboratory 3-Dimensional (CFL3D)LAR-16003-1CFL3D is a structured-grid, cell-centered, upwind-biased, Reynolds-averaged Navier-Stokes (RANS) code.It can be run in parallel on multiple grid zones with point-matched, patched, overset, or embedded connectivities.Both multigrid and mesh sequencing are available in time-accurate or steady-state modes.U.S. Release Only10. Design and Integration ToolsConfiguration-Based Aerodynamics (CBAero)ARC-15819-1CBAero is a software tool for the prediction of the conceptual aero-thermodynamic environments of aerospaceconfigurations. The vehicle geometry is defined using unstructured, triangulated surface meshes. For subsonicMach numbers a fast, unstructured, multi-pole panel code is coupled with a streamline tracing formulation todefine the viscous surface solution. For supersonic and hypersonic Mach numbers, various independent panelmethods are coupled with the streamline tracing formulation, attachment line detection methods, and stagnation-attachmentline heating models to define the viscous aero-thermal environment.U.S. Government Purpose ReleaseCOPERNICUS Generalized Methodology for Designing Spacecraft TrajectoriesMSC-24209-1COPERNICUS provides a single, unified framework for modeling, designing, and optimizing spacecrafttrajectories for robotic and human missions. The methodology facilitates modeling and optimization forproblems ranging from a single spacecraft orbiting a single celestial body to a mission involving multiplespacecraft and multiple propulsion systems operating in gravitational fields of multiple celestial bodies.U.S. Government Purpose Release86NASA Technology Transfer Program Software Catalog 2014