F02K 9/766
With liquid propellant
Official title: {with liquid propellant}
F02K9/766 (With liquid propellant) appears on 16 US grants and 9 published applications in this corpus.
Search patents in F02K- Granted patents
- 16
- Published applications
- 9
- Assignees
- 13
- Inventors
- 33
- Latest grant
- 8 Nov 2016
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 1 | 0 |
| 1977 | 0 | 0 |
| 1978 | 0 | 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 | 0 | 0 |
| 1991 | 0 | 0 |
| 1992 | 2 | 0 |
| 1993 | 1 | 0 |
| 1994 | 0 | 0 |
| 1995 | 0 | 0 |
| 1996 | 1 | 0 |
| 1997 | 0 | 0 |
| 1998 | 1 | 0 |
| 1999 | 0 | 0 |
| 2000 | 0 | 0 |
| 2001 | 1 | 0 |
| 2002 | 1 | 2 |
| 2003 | 1 | 2 |
| 2004 | 3 | 0 |
| 2005 | 1 | 1 |
| 2006 | 0 | 0 |
| 2007 | 0 | 0 |
| 2008 | 0 | 0 |
| 2009 | 0 | 0 |
| 2010 | 0 | 1 |
| 2011 | 0 | 1 |
| 2012 | 0 | 0 |
| 2013 | 0 | 0 |
| 2014 | 1 | 0 |
| 2015 | 0 | 1 |
| 2016 | 2 | 0 |
| 2017 | 0 | 0 |
| 2018 | 0 | 0 |
| 2019 | 0 | 0 |
| 2020 | 0 | 0 |
| 2021 | 0 | 0 |
| 2022 | 0 | 0 |
| 2023 | 0 | 0 |
| 2024 | 0 | 1 |
By publication year. Applications have been published since 2001.
Recent patents
- Spacecraft fitted with a de-orbiting device comprising a detonation engine8 Nov 2016US 9,487,310 B2Snecma
- Glow plug type acoustic resonance igniter25 Oct 2016US 9,476,399 B1Orbital Technologies Corporation
- Cryogenic tank and space launcher including such a tank8 Apr 2014US 8,690,000 B2L Air Liquide, Societe Anonyme Pour L'Etude et L'Exploitation des Procedes Georges Claude
- Axisymmetric, throttleable non-gimballed rocket engine15 Nov 2005US 6,964,154 B1The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
- Method for placing payload in orbit by multifunctional launch vehicle of combined scheme with cruise liquid rocket engine system (lres), multifunctional launch vehicle of combined scheme with cruise lres and method for refining it3 Aug 2004US 6,769,651 B2Federalnoe Gosudarstvennoe Unitarnoe Predpriyatie Gosudarstvenny Kosmichesky Nauchno-Proizvodstvenny Tsentr IM.M.V. Krunicheva
- Aerospike engines, launch vehicles incorporating such engines and methods29 Feb 2024US 2024/0067362 A1Pangea Aerospace, S.L.
- Spacecraft fitted with a de-orbiting device comprising a detonation engine28 May 2015US 2015/0144738 A1Snecma
- Cryogenic Tank and Space Launcher Including Such a Tank1 Dec 2011US 2011/0289942 A1L'Air Liquide Societe Anonyme Pour L'Etude Et L'Explicitation Des Procedes Georges Claude
- Multiple-use rocket engines and associated systems and methods30 Dec 2010US 2010/0326045 A1Blue Origin, LLC
- Rocket engine passivation system3 Feb 2005US 2005/0022500 A1
Most cited
By later US patents
- Two stage launch vehicle and launch trajectory method66US 5,568,901 A1996
- Launch vehicle with interstage propellant manifolding38US 5,141,181 A1992
- Launch vehicle with reconfigurable interstage propellant manifolding and solid rocket boosters33US 5,143,328 A1992
- Glow plug type acoustic resonance igniter25US 9,476,399 B1Orbital Technologies Corporation · 2016
- Multiple payload/failure mode launch vehicles22US 5,203,844 A1993