Rocket nozzles for unconventional vehicles

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 8186145
APP PUB NO 20090211258A1
SERIAL NO

12072487

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Abstract

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Improved rocket nozzle designs for vehicles with nozzles embedded in or protruding from surfaces remote from the desired thrust axis. The nozzle configurations are for rocket vehicles where the nozzles are not located at the optimal thrust axis of the vehicle. Two examples include nozzles located on the forward end of the vehicle (also called tractor nozzles) and attitude control nozzles located on the periphery of the vehicle. More particularly, the disclosed nozzle shapes enhance the axial thrusts and/or maneuver torques on the vehicle. These unconventional nozzle shapes improve vehicle performance.

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Patent Owner(s)

Patent OwnerAddress
AEROJET ROCKETDYNE INCP O BOX 13222 SACRAMENTO CA 95813-6000

International Classification(s)

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  • 2008 Application Filing Year
  • F02K Class
  • 198 Applications Filed
  • 143 Patents Issued To-Date
  • 72.23 % Issued To-Date
Click to zoom InYear of Issuance% of Matters IssuedCumulative IssuancesYearly Issuances200820092010201120122013201420152016201720180255075100

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bulman, Melvin J Orangevale, US 34 300

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Citation count rangeNumber of patents cited in rangeNumber of patents cited in various citation count ranges241163401 - 1011 - 2021 - 3031 - 4002.557.51012.51517.52022.52527.53032.53537.54042.545

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