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Analytical investigation of an acceleration autopilot for control of the impact point of a ballistic missile during reentry

By Carney, T. M.

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Book Id: WPLBN0002201310
Format Type: PDF eBook :
File Size: 11.1 MB
Reproduction Date: 2012

Title: Analytical investigation of an acceleration autopilot for control of the impact point of a ballistic missile during reentry  
Author: Carney, T. M.
Volume:
Language: English
Subject: BLUFF BODIES, BODIES OF REVOLUTION, PITCHING MOMENTS
Collections: NASA Publication Collection
Historic
Publication Date:
1961
Publisher:

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M, C. T., & H, L. J. (1961). Analytical investigation of an acceleration autopilot for control of the impact point of a ballistic missile during reentry. Retrieved from http://worldpubliclibrary.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: BLUFF BODIES; BODIES OF REVOLUTION; PITCHING MOMENTS; BOUNDARY LAYER TRANSITION; DAMPING; PITCH (INCLINATION); REYNOLDS NUMBER; SUPERSONIC WIND TUNNELS

 

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