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A restraint system enabling pilot control under moderately high acceleration in a varied acceleration field

By Smedal, Harald A.

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Book Id: WPLBN0002207807
Format Type: PDF eBook :
File Size: 23.2 MB
Reproduction Date: 2012

Title: A restraint system enabling pilot control under moderately high acceleration in a varied acceleration field  
Author: Smedal, Harald A.
Volume:
Language: English
Subject: AERODYNAMIC HEATING, SPACECRAFT SHIELDING, ATMOSPHERIC ENTRY SIMULATION
Collections: NASA Publication Collection
Historic
Publication Date:
1960
Publisher:

Citation

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A, S. H., C, I. R., & W, S. G. (1960). A restraint system enabling pilot control under moderately high acceleration in a varied acceleration field. Retrieved from http://ebook2.worldlibrary.net/


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: AERODYNAMIC HEATING; SPACECRAFT SHIELDING; ATMOSPHERIC ENTRY SIMULATION; THERMAL STRESSES; TEMPERATURE EFFECTS; THERMAL ANALYSIS; REENTRY SHIELDING; REENTRY TRAJECTORIES; SCALE MODELS; SPACECRAFT REENTRY; ABLATION; HEAT SINKS; LIFTING BODIES

 

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