Ammunition and explosives – Having reaction motor
Patent
1995-08-15
1997-10-14
Tudor, Harold J.
Ammunition and explosives
Having reaction motor
60253, 244 31, 244 321, 244 324, 244130, F42B 1500
Patent
active
056775083
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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"Rocket Propulsion Elements" by George P. Sutton, 1963 p. 360.
Connel Tim S.
Finn Kevin P.
Oh Youn H.
Schwartz, II Homer H.
Snyder Richard J.
Brown Charles D.
Denson-Low Wanda K.
Hughes Missile Systems Company
Tudor Harold J.
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