OXIDIZER-RICH LIQUID MONOPROPELLANTS FOR A DUAL MODE CHEMICAL ROCKET ENGINE

The subject invention relates to oxidizer-rich liquid monopropellants based on ADN or HAN for a dual mode bipropellant chemical rocket engine. Such engines may be part of propulsion systems to be used in aerospace applications for 1) orbit raising, orbit manoeuvres and maintenance, attitude control...

Full description

Saved in:
Bibliographic Details
Main Authors THORMÄHLEN PETER, ANFLO KJELL
Format Patent
LanguageEnglish
Published 31.03.2016
Subjects
BLASTING
CHEMISTRY
COMBUSTION ENGINES
EXPLOSIVES
EXPLOSIVES OR THERMIC COMPOSITIONS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MANUFACTURE THEREOF
MATCHES
MECHANICAL ENGINEERING
METALLURGY
USE OF SINGLE SUBSTANCES AS EXPLOSIVES
WEAPONS
Online AccessGet full text

Cover

More Information
Summary:The subject invention relates to oxidizer-rich liquid monopropellants based on ADN or HAN for a dual mode bipropellant chemical rocket engine. Such engines may be part of propulsion systems to be used in aerospace applications for 1) orbit raising, orbit manoeuvres and maintenance, attitude control and deorbiting of spacecraft, and/or 2) propellant settling, attitude and roll control of missiles, launchers and space planes.
Bibliography:Application Number: US201414892033