Missile having non-cylindrical propulsion section
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United States of America Patent
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Oct 14, 1997
Grant Date -
N/A
app pub date -
Aug 15, 1995
filing date -
Aug 15, 1995
priority date (Note) -
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Abstract
A missile has a non-cylindrical fuselage over at least a portion of its length, with a non-cylindrical propulsion system contained within the non-cylindrical portion of the fuselage. The fuselage and propulsion system are preferably generally elliptical in cross section, with a dimensional ratio of the major axis to the minor axis of from more than 1:1 to about 1.5:1. The missile further includes a guidance system and guidance control features.
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