C06B 47/06
A component being a liquefied normally gaseous material supplying oxygen
Official title: a component being a liquefied normally gaseous material supplying oxygen (C06B47/04 takes precedence)
C06B47/06 (A component being a liquefied normally gaseous material supplying oxygen) appears on 13 US grants and 3 published applications in this corpus.
Search patents in C06B- Granted patents
- 13
- Published applications
- 3
- Assignees
- 10
- Inventors
- 34
- Latest grant
- 26 Dec 2023
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1978 | 1 | 0 |
| 1979 | 0 | 0 |
| 1980 | 0 | 0 |
| 1981 | 0 | 0 |
| 1982 | 0 | 0 |
| 1983 | 0 | 0 |
| 1984 | 0 | 0 |
| 1985 | 0 | 0 |
| 1986 | 0 | 0 |
| 1987 | 0 | 0 |
| 1988 | 0 | 0 |
| 1989 | 0 | 0 |
| 1990 | 1 | 0 |
| 1991 | 0 | 0 |
| 1992 | 1 | 0 |
| 1993 | 0 | 0 |
| 1994 | 0 | 0 |
| 1995 | 0 | 0 |
| 1996 | 0 | 0 |
| 1997 | 1 | 0 |
| 1998 | 1 | 0 |
| 1999 | 0 | 0 |
| 2000 | 1 | 0 |
| 2001 | 3 | 0 |
| 2002 | 2 | 0 |
| 2003 | 1 | 1 |
| 2004 | 0 | 0 |
| 2005 | 0 | 0 |
| 2006 | 0 | 0 |
| 2007 | 0 | 0 |
| 2008 | 0 | 0 |
| 2009 | 0 | 0 |
| 2010 | 0 | 0 |
| 2011 | 0 | 0 |
| 2012 | 0 | 0 |
| 2013 | 0 | 0 |
| 2014 | 0 | 0 |
| 2015 | 0 | 0 |
| 2016 | 0 | 0 |
| 2017 | 0 | 1 |
| 2018 | 0 | 0 |
| 2019 | 0 | 1 |
| 2020 | 0 | 0 |
| 2021 | 0 | 0 |
| 2022 | 0 | 0 |
| 2023 | 1 | 0 |
By publication year. Applications have been published since 2001.
Recent patents
- Flexible halocarbon pyrolant26 Dec 2023US 11,851,382 B1The United States of America as represented by the Secretary of the Navy
- Reduced toxicity fuel satellite propulsion system including plasmatron15 Apr 2003US 6,546,714 B1The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
- Method for increasing the specific impulse in a liquid-propellant rocket engine and rocket powder unit for realising the same9 Jul 2002US 6,415,596 B1Otkrytoe Aktsionernoe Obschestvo ″NPO Energomash imeni akademika V.P.
- Reduced toxicity fuel satellite propulsion system including catalytic decomposing element with hydrogen peroxide30 Apr 2002US 6,378,291 B1The United States of America as represented by the Administrator of the National Aeronatics and Space Administration
- Reduced toxicity fuel satellite propulsion system including fuel cell reformer with alcohols such as methanol13 Nov 2001US 6,314,718 B1The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
Most cited
By later US patents
- Liquid-fueled inflator with a porous containment device35US 5,607,181 AMorton International, Inc. · 1997
- Liquid-solid propulsion system and method32US 5,099,645 AGeneral Dynamics Corporation, Space Systems Division · 1992
- Reduced toxicity fuel satellite propulsion system22US 6,272,846 B1The United States of America as represented by the Administrator of the National Aeronautics and Space Administration · 2001
- Cryogenic propellants and method for producing cryogenic propellants12US 5,705,771 A1998
- Reduced toxicity fuel satellite propulsion system including axial thruster and ACS thruster combination9US 6,311,477 B1The United States of America as represented by the Administrator of the National Aeronautics and Space Administration · 2001