Folding tail fins
First Claim
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1. A flip out tail assembly for a missile comprising:
- Pairs of lugs extending rearwardly from said missile, said missile having a diagonal flat surface at the rear thereof;
four fins each having a hinged hub portion pivotally secured between said pair of lugs, each said hinged hub portion having a first flat surface and a second flat surface inclined at an angle thereto, a lug disposed on said second flat surface and projecting upwardly therefrom;
a plunger slidably mounted in the rear of said missile adjacent each said pair of lugs;
each said plunger having an outwardly facing flat surface having a recess at the rearmost end thereof;
spring means for biasing said plunger against said hinged hub portion whereby said fin is pivoted outwardly so that said lug on said hinged hub portion enters said recess on said plunger and said first flat surface of said hub portion engages said diagonal surface of the rearend of said missile for retention of said fin in the extended position; and
a shroud assembly fixed to said missile and having four longitudinal slots formed therein through which the fins are adapted to project.
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Abstract
A rocket having flip out tail fins with cooperating surfaces on said fins d the rear of said rocket to maintain said fins in extended position. Spring means for urging said cooperating surfaces into engagement with each other.
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Citations
1 Claim
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1. A flip out tail assembly for a missile comprising:
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Pairs of lugs extending rearwardly from said missile, said missile having a diagonal flat surface at the rear thereof; four fins each having a hinged hub portion pivotally secured between said pair of lugs, each said hinged hub portion having a first flat surface and a second flat surface inclined at an angle thereto, a lug disposed on said second flat surface and projecting upwardly therefrom; a plunger slidably mounted in the rear of said missile adjacent each said pair of lugs;
each said plunger having an outwardly facing flat surface having a recess at the rearmost end thereof;spring means for biasing said plunger against said hinged hub portion whereby said fin is pivoted outwardly so that said lug on said hinged hub portion enters said recess on said plunger and said first flat surface of said hub portion engages said diagonal surface of the rearend of said missile for retention of said fin in the extended position; and a shroud assembly fixed to said missile and having four longitudinal slots formed therein through which the fins are adapted to project.
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Specification
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Current AssigneeUnited States Of America As Represented By The Secretary Of The Army (Government of the United States of America)
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Original AssigneeThe United States Of America As Represented By The Secretary Of The Army
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InventorsHowlett, Donald E., Marburger, Ivan L., Nagel, Lawrence J.
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Primary Examiner(s)Pendegrass, Verlin R.
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Application NumberUS05/637,601Time in Patent Office383 DaysField of Search244/3.27, 244/3.28, 244/3.29US Class Current244/3.28CPC Class CodesF42B 10/14 using fins spread or deploy...
