Instrumentation applications to Space Shuttle models and thermal protection system tiles tested in NASA-AMES wind tunnelsThe highlights of the many wind-tunnel tests conducted in the course of the Space Shuttle development program are presented with emphasis on instrumentation applications. The examples of tests discussed include airframe aerodynamics, aerodynamic heating, aerodynamic noise, tile dynamic response, and tile loads. Many of the tests were conducted with standard wind-tunnel instrumentation. Most of the more unusual instrumentation requirements were related to the thermal protection system, where some pressure-sensor concepts were adapted to measure airloads on tiles. These measurements provided the only quantitative data that could be used to confirm the airload analysis procedure. Limited applications of computers to experimental control, in conjunction with data taken during Shuttle tests, have resulted in substantial benefits in overall test efficiency.
Document ID
19830029847
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Coe, C. F. (NASA Ames Research Center Moffett Field, CA, United States)
Brownson, J. J. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1981
Subject Category
Ground Support Systems And Facilities (Space)
Meeting Information
Meeting: ICIASF ''81; International Congress on Instrumentation in Aerospace Simulation Facilities