US2003194943A1PendingUtilityA1
Model rocket motor retainer apparatus
Priority: Apr 16, 2002Filed: Apr 16, 2002Published: Oct 16, 2003
Est. expiryApr 16, 2022(expired)· nominal 20-yr term from priority
A63H 27/005
40
PatentIndex Score
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Claims
Abstract
A model rocket motor retainer apparatus for model rockets comprised of two components, a cylindrical retainer body ( 1 ) and an aft closure ring ( 2 ); wherein the retainer body is attached to a rocket motor tube ( 3 ), and the aft closure ring attaches into the aft end of the retainer body ( 3 ). Installation and tightening of the aft closure ring traps the rocket motor ( 4 ) between the aft closure ring and the rocket motor tube, thereby positively retaining the motor.
Claims
exact text as granted — not AI-modifiedI claim:
1 . A model rocket motor retainer apparatus comprising a retainer body and an aft closure ring attached to said retainer body, as a means for retaining a model rocket motor within a rocket airframe.
2 . A model rocket motor retainer apparatus per claim 1 wherein said aft closure ring further includes appropriately sized through-bores as a means to accommodate rocket model motors of various sizes.
3 . A model rocket motor retainer apparatus per claim 1 wherein said retainer body further includes a minimal outside diameter as a means to provide improved aerodynamic characteristics through drag reduction.
4 . A model rocket motor retainer apparatus per claim 1 wherein said retainer body further includes internal threading on the aft inside diameter as a means to accommodate rocket motors with rear thrust rings of varying lengths.
5 . A model rocket motor retainer apparatus per claim 1 wherein said retainer body further includes an outer conical, ogive, or similar contour, that aerodynamically transitions from a rocket motor tube diameter to an airframe tube diameter for use on rockets with an airframe tube of larger diameter than the motor tube.
6 . A model rocket motor retainer apparatus per claim 1 wherein said retainer body further includes an outer contour shaped to simulate a larger model rocket motor with a thrust ring as a means for adapting smaller rocket motors for installation in larger motor tubes.Join the waitlist — get patent alerts
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