NASA_Software_Catalog_2014.pdf#sthash.Rk7M8wlL

Computed Tomography Cylinder Unwrapper/Re-slicer Software (CT-CURS), Version 2LEW-19031-1CT-CURS is a dedicated unwrapping/re-slicing software tool for computing tomography data from cylindricaland partially cylindrical structures. The technology can be used as a complement to vendor software or can beutilized as a completely standalone visualization program.U.S. Release OnlyController CodeLEW-17293Written in C++, this technology is a comprehensive controller for magnetically supported vertical rotors.U.S. Release OnlyCORBASecThis technology has been used for distributed aerospace propulsion simulations.U.S. Release OnlyLEW-17214Cryogen Storage Integrated Model (CryoSIM)MFS-33071-1CryoSIM provides input power and dry mass estimates for insulation and hardware used in in-space applicationsto maintain cryogens in storage. System heat load estimations and associated propellant lossmasses can also be generated.U.S. Government Purpose ReleasePropellant Feed System Analytical Tool (PFSAT)MSC-25181-1The PFSAT parametric analytical tool predicts heat leaks into cryogenic propellant distribution lines. The technologycan also be used to determine the optimum orifice diameter for an optional thermodynamic vent system.U.S. Government Purpose ReleaseCSPAN Axial-Flow Compressor Conceptual Design CodeThis span-line analysis technology uses isentropic simple radial equilibrium to determine a flow path.U.S. Government Purpose ReleaseExtended Testability Analysis (ETA) ToolLEW-16074LEW-18795-1ETA extends the analysis capabilities of Qualtech Systems’ Testability Engineering and Maintenance System(TEAMS), a technology that enables a user to qualitatively model and analyze fault propagation.U.S. Release OnlyFModel6 Redesigned Solid Rocket Motor (RSRM) Steady-State and Tail-offTransient Dispersions AlgorithmThis Fortran 77 mathematical algorithm has been used to model steady-state and tail-off RSRMcharacteristics.U.S. Government Purpose ReleaseGaseous Nitrogen (GN2) Orifice Mass-Flow CalculatorMSC-25204-1MSC-24873-1This calculator has been used to determine GN2 high-pressure tank-source depletion rates for the SpaceShuttle Orbiter Water Spray Boiler (WSB), and it has also been used to gauge the ability of GN2 consumablesto support APU lubrication cooling during entry.U.S. Government Purpose Release5. PropulsionLiquid Oxygen (LO2) De-tanking Pressure Surge Prediction ProgramMSC-25207-1This technology defines the LO2 feed system and ground system pressure surges that result from de-tankinginto a reverted tail service mast (TSM). The software can simulate a Main Propulsion System (MPS) LO2inboard fill and drain valve; ground helium supply; and/or anti-geyser helium supply.U.S. Government Purpose Release44NASA Technology Transfer Program Software Catalog 2014