Iridium-catalyzed hydrogen peroxide based monopropellant system
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
N/A
Issued Date -
Nov 4, 2004
app pub date -
Mar 31, 2003
filing date -
Mar 31, 2003
priority date (Note) -
Abandoned
status (Latency Note)
Importance
Abstract
Rocket propulsion or rapid response gas generation systems and methods are disclosed in which a novel one component, single tank storable, low toxicity, low detonation sensitivity liquid monopropellant containing a mixture of aqueous 70% hydrogen peroxide, alcohol, and water is catalytically decomposed with an iridium based catalyst. The resulting rapidly formed gaseous decomposition products consisting substantially of carbon dioxide and water vapor are used for rocket propulsion, satellite propulsion, divert attitude control systems for interceptor missiles, and other power control systems where a re-start capability is desired.
First Claim
Family
International Classification(s)
Cited Art Landscape
Patent Citation Ranking
Recipient Email Address
Recipient Email Address
Comment
Recipient Email Address
Add to Portfolio(s)
To add this patent to one, or more, of your portfolios, simply click the add button.
This Patent is in these Portfolios:
Add to additional portfolios:
Last Refreshed On:
Changes done successfully