NDLI: Users guide: steady-state aerodynamic-loads program for shuttle tps tiles

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Users guide: steady-state aerodynamic-loads program for shuttle tps tiles

Content Provider	NASA Technical Reports Server (NTRS)
Author	Kerr, P. A. Petley, D. H.
Copyright Year	1984
Description	A user's guide for the computer program that calculates the steady-state aerodynamic loads on the Shuttle thermal-protection tiles is presented. The main element in the program is the MITAS-II, Martin Marietta Interactive Thermal Analysis System. The MITAS-II is used to calculate the mass flow in a nine-tile model designed to simulate conditions duing a Shuttle flight. The procedures used to execute the program using the MITAS-II software are described. A list of the necessry software and data files along with a brief description of their functions is given. The format of the data file containing the surface pressure data is specified. The interpolation techniques used to calculate the pressure profile over the tile matrix are briefly described. In addition, the output from a sample run is explained. The actual output and the procedure file used to execute the program at NASA Langley Research Center on a CDC CYBER-175 are provided in the appendices.
File Size	4131751
Page Count	116
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19860017934
Archival Resource Key	ark:/13960/t2z36np9h
Language	English
Publisher Date	1984-07-01
Access Restriction	Open
Subject Keyword	Spacecraft Design, Testing And Performance Space Shuttles Reusable Heat Shielding Steady State User Manuals Computer Programs Format Thermal Protection Tiles Applications Programs Computers Thermal Analysis Pressure Measurement Heat Transfer Mass Flow Aerodynamic Loads Software Engineering Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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