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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 |
| 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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