Inventor · disambiguated record
Allan P. Thompson
Also filed as: SHIGLEY JOHN K · THOMPSON ALLAN · THOMPSON ALLAN P
6 granted patents·1 pending application·23 citations·filing 1988–2016
77Inventor score
Files withCORDANT TECH INC2ALLIANT TECHSYSTEMS INC1HOLLINGSWORTH UK LTD1NORTHROP GRUMMAN INNOVATION SYSTEMS INC1WILSON KENNETH P1
Top patents by PatentIndex Score
7 records- 0146US10815936B2Flexible bearing assemblies, rocket motors including such assemblies, and methods of forming flexible bearingsNORTHROP GRUMMAN INNOVATION SYSTEMS INC·Filed 2016·Granted Oct 27, 2020·0 cites·18 claims
- 0244US2004105970A1Low density composite rocket nozzle components and process for making the same from standard density phenolic matrix, fiber reinforced materialsFiled 2003·Application pending·0 cites
- 0343US6235359B1Rocket assembly ablative materials formed from, as a precursor, staple cellulosic fibers, and method of insulating or thermally protecting a rocket assembly with the sameCORDANT TECH INC·Filed 1999·Granted May 22, 2001·9 cites·20 claims
- 0439US6679965B1Low density composite rocket nozzle components and process for making the same from standard density phenolic matrix, fiber reinforced materialsALLIANT TECHSYSTEMS INC·Filed 1998·Granted Jan 20, 2004·8 cites·31 claims
- 0538US4884394AFriction spinning unit and method of operating sameHOLLINGSWORTH UK LTD·Filed 1988·Granted Dec 5, 1989·2 cites·20 claims
- 0632USRE43867ERocket assembly ablative materials formed from, as a precursor, staple cellulosic fibers, and method of insulating or thermally protecting a rocket assembly with the sameWILSON KENNETH P·Filed 2003·Granted Dec 18, 2012·0 cites·22 claims
- 0731US6479148B1Rocket assembly ablative materials formed from solvent-spun cellulosic precursors, and method of insulating or thermally protecting a rocket assembly with the sameCORDANT TECH INC·Filed 1999·Granted Nov 12, 2002·4 cites·19 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →