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Inertial guidance system design requirements for short range missile applications
Thesis

Inertial guidance system design requirements for short range missile applications

John F. Muller
Master of Science (M.S.), Drexel Institute of Technology
1965
DOI:
https://doi.org/10.17918/00005958
pdf
Muller_John_196586.68 MB
PDF Restricted Access, VIEWABLE UPON REQUEST: contact archives@drexel.edu

Abstract

Inertial navigation (Astronautics)

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