Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Liquid propellant rocket engine with parallel auxiliary flow, and an integrated gas generator

Liquid propellant rocket engine with parallel auxiliary flow, and an integrated gas generator

US Patent 5404715 · Granted Apr 11, 1995

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Tank for a spacecraft engine2022
Device for pressurizing a propellant tank of a rocket engine2019
Propellant feed circuit and a cooling method2018
Device for heating a fluid2017
Cryogenic thruster assembly using regenerative heating from main and settling th2016
Rocket engine nozzle system2012
Device for displacing to nozzle outlet or eliminating jet separation in rocket e2003
Method of manufacturing a combustion enclosure with cooling by transpiration1999
Injection system and an associated tricoaxial element1999
Combustion enclosure with cooling by transpiration1998
Injection system and an associated tricoaxial element1997
Injection system with concentric slits and the associated injection elements1997