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Results of tests on a 0.04 scale Space Shuttle Orbiter forebody model (83-0) in the AEDC VKF hypersonic wind tunnel B to obtain aerodynamic heating distribution on lower fuselage and RCS nozzle area (OH103A)

By Lemoine, P. L.

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Book Id: WPLBN0002206098
Format Type: PDF eBook :
File Size: 12.0 MB
Reproduction Date: 2012

Title: Results of tests on a 0.04 scale Space Shuttle Orbiter forebody model (83-0) in the AEDC VKF hypersonic wind tunnel B to obtain aerodynamic heating distribution on lower fuselage and RCS nozzle area (OH103A)  
Author: Lemoine, P. L.
Volume:
Language: English
Subject: CREEP PROPERTIES, TANTALUM ALLOYS, DUCTILITY
Collections: NASA Publication Collection
Historic
Publication Date:
1982
Publisher:

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L, L. P., & R, N. J. (1982). Results of tests on a 0.04 scale Space Shuttle Orbiter forebody model (83-0) in the AEDC VKF hypersonic wind tunnel B to obtain aerodynamic heating distribution on lower fuselage and RCS nozzle area (OH103A). Retrieved from http://cn.ebooklibrary.org/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents

Summary
Contributor: National Aeronautics and Space Administration (NASA). The digitalization of this book was sponsored by National Aeronautics and Space Administration (NASA); Additional Subject Descriptions: CREEP PROPERTIES; TANTALUM ALLOYS; DUCTILITY; CRACK PROPAGATION; COMPRESSION LOADS; CRACK INITIATION; GRAIN BOUNDARIES; PLASTIC DEFORMATION; SLIDING; TENSILE STRESS; CYCLIC LOADS; FRACTURING; HEAT RESISTANT ALLOYS; METAL FATIGUE

 
 



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