F42B 10/30
Using rocket motor nozzles
Official title: using rocket motor nozzles
F42B10/30 (Using rocket motor nozzles) appears on 33 US grants and 13 published applications in this corpus.
Search patents in F42B- Granted patents
- 33
- Published applications
- 13
- Assignees
- 21
- Inventors
- 60
- Latest grant
- 3 Mar 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 2 | 0 |
| 1977 | 2 | 0 |
| 1978 | 1 | 0 |
| 1979 | 0 | 0 |
| 1980 | 3 | 0 |
| 1981 | 0 | 0 |
| 1982 | 0 | 0 |
| 1983 | 0 | 0 |
| 1984 | 0 | 0 |
| 1985 | 1 | 0 |
| 1986 | 1 | 0 |
| 1987 | 0 | 0 |
| 1988 | 1 | 0 |
| 1989 | 0 | 0 |
| 1990 | 0 | 0 |
| 1991 | 0 | 0 |
| 1992 | 1 | 0 |
| 1993 | 0 | 0 |
| 1994 | 0 | 0 |
| 1995 | 0 | 0 |
| 1996 | 0 | 0 |
| 1997 | 2 | 0 |
| 1998 | 0 | 0 |
| 1999 | 1 | 0 |
| 2000 | 0 | 0 |
| 2001 | 0 | 0 |
| 2002 | 2 | 0 |
| 2003 | 0 | 1 |
| 2004 | 1 | 0 |
| 2005 | 1 | 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 | 1 | 1 |
| 2015 | 2 | 0 |
| 2016 | 1 | 4 |
| 2017 | 1 | 2 |
| 2018 | 2 | 1 |
| 2019 | 0 | 0 |
| 2020 | 3 | 1 |
| 2021 | 1 | 0 |
| 2022 | 0 | 2 |
| 2023 | 1 | 0 |
| 2024 | 1 | 1 |
| 2025 | 0 | 0 |
| 2026 | 1 | 0 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Recent patents
- Maneuvering aeromechanically stable sabot system3 Mar 2026US 12,566,054 B2University of Kansas
- Trajectory shaping2 Apr 2024US 11,946,727 B2Israel Aerospace Industries Ltd.
- Maneuvering aeromechanically stable sabot system26 Dec 2023US 11,852,447 B2University of Kansas
- Projectile apparatus for smooth bore barrels4 May 2021US 10,996,033 B2
- Deflector for a thrust flow powered vehicle and thrust flow powered vehicle with said deflector15 Sep 2020US 10,774,785 B2Mbda UK Limited
- Maneuvering aeromechanicaly stable sabot system30 May 2024US 2024/0175666 A1University of Kansas
- Trajectory shaping13 Oct 2022US 2022/0325993 A1Israel Aerospace Industries Ltd.
- Maneuvering aeromechanically stable sabot system11 Aug 2022US 2022/0252382 A1University of Kansas
- Projectile Apparatus For Smooth Bore Barrels20 Feb 2020US 2020/0056866 A1
- High Spin Projectile Apparatus Comprising Components Made by Additive Manufacture7 Jun 2018US 2018/0154446 A1
Most cited
By later US patents
- Directional control of missiles31US 6,889,935 B2Metal Storm Limited · 2005
- Mechanical roll rate stabilizer for a rolling missile23US 4,029,270 AGeneral Dynamics Corporation · 1977
- Missiles19US 4,745,861 ABritish Aerospace PLC · 1988
- Rocket-propelled grenade16US 9,068,807 B1Lockheed Martin Corporation · 2015
- Method of controlling the spin rate of tube launched rockets15US 3,964,696 AThe United States of America as represented by the Secretary of the Navy · 1976