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Browse by Category: Main > Firearms & Weapons
Class Information
Number: 102/381
Name: Ammunition and explosives > Having reaction motor > Having pressurization or variable control means for the propellant
Description: Subject matter including means for (a) the pressurization of a fluid propelling means of the reaction motor, or (b) the variable control or regulation of the propellent charge of the reaction motor during the flight of the missile so that the degree of combustion of the motor propellant or the time of combustion of such propellant may be regulated.










Patents under this class:

Patent Number Title Of Patent Date Issued
8453572 Gun fired propellant support assemblies and methods for same Jun. 4, 2013
8402895 Vortice amplified diffuser for buoyancy dissipater and method for selectable diffusion Mar. 26, 2013
7895948 Buoyancy dissipater and method to deter an errant vessel Mar. 1, 2011
7836827 Method of operating a supercavitating projectile based on time constraints Nov. 23, 2010
7832336 Method of operating a supercavitating projectile based on velocity constraints Nov. 16, 2010
7730838 Buoyancy dissipater and method to deter an errant vessel Jun. 8, 2010
7578238 Base bleed boat tail converter for projectile Aug. 25, 2009
7347146 Supercavitating projectile with propulsion and ventilation jet Mar. 25, 2008
7051659 Projectile structure May. 30, 2006
6966264 Rocket motors with insensitive munitions systems and projectiles including same Nov. 22, 2005
6873945 Rocket motor propellant temperature simulator Mar. 29, 2005
6619029 Rocket motors with insensitive munitions systems Sep. 16, 2003
6536350 Stagnation pressure activated fuel release mechanism for hypersonic projectiles Mar. 25, 2003
6125763 Integral solid booster and hybrid thrust sustaining system and projectile incorporating the same Oct. 3, 2000
6094906 Design for a gun-launched rocket Aug. 1, 2000
5817968 Gas generation with high pressure sensitivity exponent propellant Oct. 6, 1998
5792981 Gun-launched rocket Aug. 11, 1998
5657948 Control of a projectile by multi-chamber and single-nozzle impeller Aug. 19, 1997
5481977 Work-controlled launching device with accumulator Jan. 9, 1996
5435128 Pyrotechnically driven nozzle restrictor Jul. 25, 1995
5054712 Projectile with correctable trajectory Oct. 8, 1991
4982913 Course correction unit Jan. 8, 1991
4803925 Device for the limitation of gas pressure in a combustion chamber provided inside a projectile Feb. 14, 1989
4723736 Rocket staging system Feb. 9, 1988
4649826 Retardation system for air launched flares and submunitions Mar. 17, 1987
4502649 Gun-launched variable thrust ramjet projectile Mar. 5, 1985
4428293 Gun-launched variable thrust ramjet projectile Jan. 31, 1984
4132165 Fuel supply system for a missile or the like Jan. 2, 1979
4095528 Vehicle with combined fuel tank/warhead Jun. 20, 1978
3999379 Reduction of depressurization thrust termination jolt Dec. 28, 1976
3946557 Rocket motor construction Mar. 30, 1976











 
 
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