Wada et al., 2016 - Google Patents
Effect of geometric swirl number of discharge plasma catalyzer on green monopropellant reaction characteristicsWada et al., 2016
View PDF- Document ID
- 300401854933256012
- Author
- Wada A
- Iizuka T
- Shindo T
- Maeda H
- Watanabe H
- Takegahara H
- Publication year
- Publication venue
- Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan
External Links
Snippet
A new reaction system that uses discharge plasma of noble gas has been proposed as a substitute for the conventional solid catalyst in a reaction control system (RCS) thruster. The propellant of the thruster is a hydroxyl ammonium nitrate (HAN)-based monopropellant …
- 238000006243 chemical reaction 0 title abstract description 76
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket- engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details
- F02K9/62—Combustion or thrust chambers
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