F42B 10/663
Using a plurality of transversally acting auxiliary nozzles, which are opened or
Official title: {using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves}
F42B10/663 (Using a plurality of transversally acting auxiliary nozzles, which are opened or) appears on 144 US grants and 51 published applications in this corpus.
Search patents in F42B- Granted patents
- 144
- Published applications
- 51
- Assignees
- 72
- Inventors
- 219
- Latest grant
- 18 Oct 2022
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 2 | 0 |
| 1977 | 3 | 0 |
| 1978 | 3 | 0 |
| 1979 | 1 | 0 |
| 1980 | 2 | 0 |
| 1981 | 0 | 0 |
| 1982 | 0 | 0 |
| 1983 | 2 | 0 |
| 1984 | 5 | 0 |
| 1985 | 7 | 0 |
| 1986 | 5 | 0 |
| 1987 | 9 | 0 |
| 1988 | 6 | 0 |
| 1989 | 4 | 0 |
| 1990 | 3 | 0 |
| 1991 | 7 | 0 |
| 1992 | 6 | 0 |
| 1993 | 1 | 0 |
| 1994 | 0 | 0 |
| 1995 | 1 | 0 |
| 1996 | 2 | 0 |
| 1997 | 4 | 0 |
| 1998 | 3 | 0 |
| 1999 | 3 | 0 |
| 2000 | 0 | 0 |
| 2001 | 6 | 0 |
| 2002 | 2 | 2 |
| 2003 | 1 | 0 |
| 2004 | 1 | 6 |
| 2005 | 4 | 2 |
| 2006 | 6 | 5 |
| 2007 | 2 | 1 |
| 2008 | 3 | 4 |
| 2009 | 2 | 1 |
| 2010 | 1 | 4 |
| 2011 | 5 | 2 |
| 2012 | 4 | 6 |
| 2013 | 2 | 1 |
| 2014 | 4 | 5 |
| 2015 | 10 | 4 |
| 2016 | 2 | 1 |
| 2017 | 1 | 0 |
| 2018 | 1 | 4 |
| 2019 | 1 | 0 |
| 2020 | 3 | 0 |
| 2021 | 2 | 2 |
| 2022 | 2 | 0 |
| 2023 | 0 | 0 |
| 2024 | 0 | 0 |
| 2025 | 0 | 0 |
| 2026 | 0 | 1 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
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- Device and system for controlling missiles and kill vehicles operated with gel-like fuels10 Aug 2021US 11,084,605 B2Bayern-Chemie Gesellschaft fur Flugchemische Antriebe mbH
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- Deflector for a thrust flow powered vehicle and thrust flow powered vehicle with said deflector15 Sep 2020US 10,774,785 B2Mbda UK Limited
- Projectile delivery systems and weaponized aerial vehicles and methods including same19 Feb 2026US 2026/0048842 A1Corvid Technologies LLC
- Kinetic energy vehicle with attitude control system having paired thrusters22 Jul 2021US 2021/0223011 A1Raytheon Company
- Kinetic energy vehicle with three-thruster divert control system22 Jul 2021US 2021/0223012 A1Raytheon Company
- A more compact side force steering and attitude control system, and a vehicle including such a system6 Dec 2018US 2018/0347957 A1Arianegroup SAS
- Projectile, and system and method for steering a projectile25 Oct 2018US 2018/0306563 A1Israel Aerospace Industries Ltd.
Most cited
By later US patents
- Solid-propellant-powered maneuvering system for spacecraft47US 5,062,593 AUnited States Government, as represented by the Secretary of the Navy · 1991
- Precision guidance system for aircraft launched bombs47US 5,507,452 ALoral Corporation · 1996
- Precision guidance system for aircraft launched bombs44US 5,657,947 ALoral Corporation · 1997
- Projectile guidance42US 3,977,629 ASociete Europeene de Propulsion · 1976
- Gas jet steering device and method missile comprising such a device39US 4,463,921 AThomson-Brandt · 1984