Orbiter entry leeside heat-transfer data analysisHeat-transfer data measured along the Space Shuttle Orbiter's leeward centerline and over the wing leeside surface during the STS-2 and STS-3 mission entries are presented. The flight data are compared with available wind-tunnel results. Flight heating levels are, in general, lower than those which are inferred from the wind-tunnel results. This result is apparently due to the flight leeside flowfield remaining laminar over a larger Reynolds number range than that of corresponding ground test results. The flight/wind-tunnel data comparisons confirm the adequacy of, and conservatism embodied in, the direct application of wind-tunnel data at flight conditions for the design of Orbiter leeside thermal protection.
Document ID
19830035527
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Throckmorton, D. A. (NASA Langley Research Center Hampton, VA, United States)
Zoby, E. V. (NASA Langley Research Center Space Systems Div., Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 83-0484
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting