Patents for F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689) |
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03/29/1988 | US4733531 Liquid-propellant management system with capillary pumping vanes |
03/23/1988 | EP0260936A2 High solids ratio solid rocket motor propellant grains and method of construction thereof |
03/22/1988 | US4732634 Method of forming threaded polar openings for composite pressure vessels |
03/15/1988 | US4730449 Radiation transfer thrusters for low thrust applications |
03/09/1988 | EP0258370A1 Reaction jet control system. |
03/08/1988 | US4729512 Rocket nozzles in layered construction |
03/08/1988 | US4729317 Concentric layer ramjet fuel |
03/03/1988 | DE3628689A1 Rocket motor |
03/02/1988 | EP0257040A1 Low pressure reaction control propulsion system for a spacecraft. |
03/01/1988 | US4727959 Assembly of large structures |
03/01/1988 | US4727902 Valve arrangement |
02/24/1988 | CN87104290A Space vehicle compound control apparatus |
02/23/1988 | US4726184 Rocket engine assembly |
02/09/1988 | US4723736 Rocket staging system |
02/02/1988 | US4722185 Double piston rocket engine assembly |
02/02/1988 | US4722183 Method for controlling the utilization of fluid bipropellant in a spacecraft rocket engine |
02/02/1988 | US4722181 Gas generator with injector mixing cup |
01/13/1988 | EP0252238A1 Liquid fuel rocket engine |
01/12/1988 | US4718238 Liquid fuel combustor |
01/05/1988 | US4716639 Method of making a hydrazine fuel injector |
12/30/1987 | WO1987007877A1 Hybrid spacecraft control system |
12/29/1987 | US4715399 Liquid-propellant management system for rockets and space vehicles |
12/23/1987 | DE3620524A1 Igniter device for rockets |
12/17/1987 | DE3620173A1 Nozzle closure |
12/16/1987 | EP0249393A2 Components for rocket engine combustion chambers |
12/15/1987 | US4712747 Homing device for guided missiles using side nozzles |
12/08/1987 | US4711086 Trident II first and second stage internal insulation |
12/08/1987 | CA1229989A1 Lateral gas jet piloting device |
12/03/1987 | WO1987007331A1 Solid propellant burn rate control device |
12/02/1987 | EP0247388A2 Rocket propulsion system having air-breathing possibilities |
12/01/1987 | USH384 Stowable three-axis reaction-steering system |
12/01/1987 | US4710641 Proportional drive servo controller with arrayed position detector |
12/01/1987 | US4709780 For connection to a rocket exhaust |
11/25/1987 | CN87103346A Rocket-engine using liquid fuel |
11/24/1987 | US4707983 Flexure disc sealed integral bipropellant valve and injector valve assembly |
11/24/1987 | US4707982 Thermal regenerative injector |
11/24/1987 | US4707981 For producing a mainstream of hot combustion gases |
11/24/1987 | US4707899 Method of making rocket motor extendible nozzle exit cone |
11/19/1987 | EP0245565A1 Steering method for a low-velocity missile, weapon system and missile therefor |
11/17/1987 | US4707225 Fluid-cooled channel construction |
11/17/1987 | US4706886 Extendible rocket-engine nozzle |
11/11/1987 | EP0244972A2 Liquid fuel combustor |
11/04/1987 | EP0244215A1 Gas thruster |
11/04/1987 | EP0243398A1 A method for controlling the utilization of fluid bipropellant in a spacecraft rocket engine. |
11/03/1987 | US4703694 Single stage autophage rocket |
11/03/1987 | US4703620 Rocket combustion chamber cooling wall of composite cooling type and method of manufacturing the same |
10/21/1987 | EP0242196A1 Thrusters |
10/21/1987 | EP0242161A2 Process for installing liner in pressure vessel |
10/13/1987 | US4698965 Hot gas source and fuel therefor |
10/06/1987 | US4697416 Motor involving the control of the mixture ratio of fuel and oxidizer for a liquid fuel motor by measuring flows, and control systems for carrying out this process |
09/30/1987 | CN87100316A Assembling equipment |
09/29/1987 | US4696233 High propellant mass fraction highly stress relieved end-burning grain structure |
09/29/1987 | US4696160 Pressure pump and injector valve system for liquid-propellant engines |
09/23/1987 | EP0238369A1 Thrust regulating device for a solid-fuel propulsion unit |
09/11/1987 | WO1987005362A1 Rocket propellant charge with negative pressure exponent |
09/02/1987 | EP0235028A1 Igniter fixable inside a rocket nozzle |
09/02/1987 | EP0234988A1 Propulsion unit combustion chamber and its assembly method |
09/02/1987 | EP0234633A2 Energetic stabilizing device for a generator of hot gases |
09/01/1987 | US4689845 Impulse propulsion unit |
08/27/1987 | WO1987004992A1 Low pressure reaction control propulsion system for a spacecraft |
08/27/1987 | WO1987004989A1 Reaction jet control system |
08/26/1987 | EP0233806A1 Nozzle with variable section |
08/25/1987 | US4688379 Gas generator |
08/19/1987 | EP0233093A1 Device for generating transverse forces on models of ballistic missiles during aerial tests |
08/19/1987 | EP0232449A2 Pressure relief valve |
08/18/1987 | US4686824 Gaseous secondary injection thrust vector control device |
08/11/1987 | US4685533 Exhaust dissipator device |
08/06/1987 | DE3633683C1 Engine test chamber (engine test rig, engine test bed) |
07/28/1987 | US4682779 Explosively driven latch/seal device |
07/28/1987 | CA1224632A1 Thermally actuated rocket motor safety system |
07/21/1987 | US4681261 Heat resistant short nozzle |
07/15/1987 | EP0228781A2 Missile expulsion motor |
07/14/1987 | US4679732 Vectorable exhaust nozzle for a gas turbine engine |
07/01/1987 | EP0227495A1 Steering device for a guided missile by means of lateral nozzles |
06/30/1987 | US4676876 Method for manufacturing components such as heat exchangers, heat absorbers, rocket engines or the like |
06/30/1987 | US4676436 Rocket motor nozzle extension system |
06/24/1987 | EP0226499A1 Internal stress relief arrangement for a solid-propulsion device, and method for its manufacture |
06/19/1987 | DE3544637A1 Filler-containing, low-smoke insulation for solid rocket propellants |
05/26/1987 | US4668583 Refractory coating |
05/20/1987 | EP0222262A1 Sealing arrangement for a turbo pump |
05/20/1987 | EP0222057A2 Pressure relief valve for a pyrotechnic gas generator |
05/20/1987 | EP0065529B1 A rocket vehicle |
05/19/1987 | US4666084 Nozzle assembly |
05/05/1987 | US4663196 Hydroxypolybutadiene reacted with diisocyanate, curing agent |
05/05/1987 | US4663065 Elastomer insulation compositions for rocket motors |
05/05/1987 | US4662964 Silicone rubber |
05/05/1987 | US4662216 Rocket exhaust probe |
04/29/1987 | EP0219561A1 Pyrotechnical charge for reducing the base drag on an artillery projectile |
04/28/1987 | CA1220961A1 Filament-wound venturi |
04/21/1987 | CA1220627A1 Thixotropic flame inhibitors for rocket propellant grains |
04/14/1987 | US4656828 Augmentation heater temperature control system |
04/09/1987 | WO1987002098A1 A method for controlling the utilization of fluid bipropellant in a spacecraft rocket engine |
04/09/1987 | DE3535779C1 Arrangement for the cooling of rocket engine walls |
04/07/1987 | US4655866 Winding on a mandrel a fringed polymer impregnated strip |
04/07/1987 | CA1220280A1 Method for burning rate characterization of solid propellants |
03/31/1987 | US4654103 Trident II baseline power embedment case bond system |
03/31/1987 | US4654097 Process for preparing bodies of rocket propulsion units |
03/24/1987 | US4652476 Reinforced ablative thermal barriers |
03/17/1987 | US4650416 NF3 combustor for cylindrical laser |
03/17/1987 | US4649823 Mechanical bond between a solid rocket propellant composition and a substrate and a method of effecting such a bond |