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Class 60/220 - Including injecting modifying fluid


Subclass of Class 60 - Power plants
Definition: Process directed to injecting a modifying fluid into the
No. of patents: 6
Last issue date: 07/04/2006


NumberTitleIssue Date
7069717Hybrid propulsion system
Disclosed is a propulsion system for a spacecraft. The propulsion system includes a supply of oxidizer and at least one nozzle. A conduit fluidly couples the supply of oxidizer and the nozzle. The conduit provides a pathway for oxidizer to flow in a downstream direc...
07/04/2006
6964699Rocket motor exhaust scrubber
A wet scrubber having a series of chambers for capturing and cooling exhaust gases generated during static test firing of rocket motors. Exhaust gas enters an inlet to a first chamber and is cooled and slowed by a spray solution. HCL gas is condensed and absorbed by...
11/15/2005
6178739Monopropellant assisted solid rocket engine
A monopropellant assisted solid rocket engine of the present invention is comprised of a combination of a solid rocket engine with nitromethane monopropellant injected into the rocket motor. By controlling the rate at which the monopropellant is injected ...
01/30/2001
5572864Solid-fuel, liquid oxidizer hybrid rocket turbopump auxiliary engine
A propulsion thruster (10) includes a solid-fuel, liquid-oxidizer main rocket engine (11), a tank (22) of liquid oxygen, and a turbine (32)-driven pump (30) for pumping liquid oxygen to the main engine. A solid-fuel, liquid-oxidizer auxiliary engine (40) ...
11/12/1996
5274998Rocket pollution reduction system
A system is provided for reducing the emissions of hydrochloric acid (HCl) from solid fuel rockets, especially during ground disposal. An aqueous solution (40, FIG. 2 ) of an alkali metal hydroxide is injected as a mist (50) into the rocket chamber (32) a...
01/04/1994
4318270Additives for suppressing the radar attenuation of rocket propellant exhaust plumes
A method for reducing radar attenuation caused by the formation of free etrons in the exhaust plume of a combusting high impulse rocket propellant which comprises contacting a microwave attenuation reducing additive having at least one element selected f...
03/09/1982
 
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