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Class Information
Number: 244/3.22
Name: Aeronautics > Missile stabilization or trajectory control > Automatic guidance > Attitude control mechanisms > Fluid reaction type
Description: Subject matter in which the mechanism for controlling attitude comprises a fluid reaction jet.
Patents under this class:
| Patent Number |
Title Of Patent |
Date Issued |
| 4913379 |
Rocket flight direction control system |
Apr. 3, 1990 |
| 4899956 |
Self-contained supplemental guidance module for projectile weapons |
Feb. 13, 1990 |
| 4867393 |
Reduced fin span thrust vector controlled pulsed tactical missile |
Sep. 19, 1989 |
| 4856734 |
Reaction jet control system |
Aug. 15, 1989 |
| 4852827 |
Apparatus for controlling a projectile |
Aug. 1, 1989 |
| 4844380 |
Detachable thrust vector mechanism for an aeronautical vehicle |
Jul. 4, 1989 |
| 4826104 |
Thruster system |
May. 2, 1989 |
| 4807529 |
Hot gas control system |
Feb. 28, 1989 |
| 4803925 |
Device for the limitation of gas pressure in a combustion chamber provided inside a projectile |
Feb. 14, 1989 |
| 4779821 |
Small vehicle roll control and steering |
Oct. 25, 1988 |
| 4765565 |
Pressure relief valve arrangement for a pyrotechnic gas generator |
Aug. 23, 1988 |
| 4763857 |
Guidance apparatus for projectiles |
Aug. 16, 1988 |
| 4762293 |
Rocket projectiles |
Aug. 9, 1988 |
| 4757960 |
Lost-fluid hydraulic actuation system |
Jul. 19, 1988 |
| 4754927 |
Control vanes for thrust vector control nozzle |
Jul. 5, 1988 |
| 4747568 |
Missile flight control system |
May. 31, 1988 |
| 4745861 |
Missiles |
May. 24, 1988 |
| 4726544 |
Projectile steering block |
Feb. 23, 1988 |
| 4712748 |
Missile |
Dec. 15, 1987 |
| 4712747 |
Homing device for guided missiles using side nozzles |
Dec. 15, 1987 |
| 4711414 |
Projectile with integrated propulsion system |
Dec. 8, 1987 |
| 4691876 |
Brake and release apparatus for a rotary nozzle body |
Sep. 8, 1987 |
| 4689845 |
Impulse propulsion unit |
Sep. 1, 1987 |
| 4685639 |
Pneumatically actuated ram air steering system for a guided missile |
Aug. 11, 1987 |
| 4684080 |
Pressure gas supply for a missile and the like |
Aug. 4, 1987 |
| 4681283 |
Apparatus for correcting the flight path of a missile |
Jul. 21, 1987 |
| 4674408 |
Ammunition article controllable during its final flight phase and method for navigation thereof towards a target |
Jun. 23, 1987 |
| 4674707 |
Apparatus for stabilizing a flying body |
Jun. 23, 1987 |
| 4662581 |
Modified null flow modulator |
May. 5, 1987 |
| 4659036 |
Missile control surface actuator system |
Apr. 21, 1987 |
| 4657208 |
Rotating warhead |
Apr. 14, 1987 |
| H236 |
Asymmetric side-exhausting nozzles |
Mar. 3, 1987 |
| 4646991 |
Controllable flow deflection system |
Mar. 3, 1987 |
| 4645139 |
Procedure for steering a low-speed missile, weapon system and missile for implementation of the procedure |
Feb. 24, 1987 |
| 4641801 |
Terminally guided weapon delivery system |
Feb. 10, 1987 |
| 4637572 |
Gas propellor for guided missile |
Jan. 20, 1987 |
| 4632336 |
Lateral gas jet piloting device |
Dec. 30, 1986 |
| 4623107 |
Regulating system for guided missiles traveling at supersonic speed |
Nov. 18, 1986 |
| 4623106 |
Reentry vehicle having active control and passive design modifications |
Nov. 18, 1986 |
| 4595157 |
Control system particularly for wingless guided ammunition |
Jun. 17, 1986 |
| 4589594 |
Thrust nozzle system |
May. 20, 1986 |
| 4579299 |
Quick turn, 90 degree omniaxial nozzle thrust control system |
Apr. 1, 1986 |
| 4573648 |
Ram air combustion steering system for a guided missile |
Mar. 4, 1986 |
| 4568040 |
Terminal guidance method and a guided missile operating according to this method |
Feb. 4, 1986 |
| 4562980 |
Rocket vehicle |
Jan. 7, 1986 |
| 4560120 |
Spin stabilized impulsively controlled missile (SSICM) |
Dec. 24, 1985 |
| 4560121 |
Stabilization of automotive vehicle |
Dec. 24, 1985 |
| 4550888 |
Dual pressure solid propellant control system |
Nov. 5, 1985 |
| 4541592 |
Wing-stabilized projectile |
Sep. 17, 1985 |
| 4537371 |
Small caliber guided projectile |
Aug. 27, 1985 |
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