Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Solid propellant burn rate, propellant gas flow rate, and propellant gas pressure pulse generation control system and method

Solid propellant burn rate, propellant gas flow rate, and propellant gas pressure pulse generation control system and method

US Patent 7886519 · Granted Feb 15, 2011

Estimated economic value: $8,397,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Aircraft thrust reverser system with alternate reverse thrust load path2019
Pneumatic taxi system2018
Air turbine starter systems including gearbox-integrated clutch modules and gas 2018
Aircraft electric taxi system diagnostic and prognostic evaluation system and me2017
Roller-based drive systems with compliance for accommodating non-conjugate meshi2017
Aircraft wheel driving system2017
Line replaceable unit health nodes and methods for determining maintenance actio2016
Aircraft landing gear wheel with integral gear drive2016
Self-snubbing hydraulic actuation system2016
Ball screw actuator including an axial soft stop2016
Aircraft selectively engageable electric taxi system2016
Active human-machine interface with force sensor overload protection2015