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4766726 |
Segmented case rocket motor
A segmented rocket motor case includes wedge members for forcing the case segments into position to remove free play at the joint thereof which may otherwise interfere with or upset the missile's...
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4756248 |
Low mass grain support system for solid propellant rocket motors
A reinforced split-flap hinge for supporting the unpressurized propellant grain of a rocket motor in a high acceleration environment includes a circular piece of material and an afterwardly spaced...
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4711086 |
Trident II first and second stage internal insulation
A rocket motor insulator of varied thickness with an integrated flap to rce propellant stresses.
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4689845 |
Impulse propulsion unit
An impulse propulsion unit or pulse-generating impeller mechanism for the lateral acceleration of a projectile, including a hollow cylindrical member, having an outer shell surface which is passed...
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4654097 |
Process for preparing bodies of rocket propulsion units
The invention relates to a process for preparing a body of a rocket propulsion unit comprising a rubber wall forming a chamber which contains a propergol and an outer wall forming reinforcement,...
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4577542 |
Dome restraint assembly for rocket motors
An adjustable restraint assembly connectable between a dome portion of a solid propellant rocket motor casing and a rigid base or support, for use during the curing of a propellant in the casing....
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4495764 |
Integrated insulation wall assembly
An integrated three-component insulation wall assembly which can be used by itself as an insulation wall assembly, or which can be incorporated into a solid rocket motor case that is made of...
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4345427 |
Rocket motor or gas generator having controlled thrust or mass flow output
A solid propellant rocket motor of gas generator of the type having retractable filaments embedded in the propellant for the purpose of controlling the overall thrust or mass flow output is...
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4314509 |
Pyrotechnic charge, with a short combustion time, comprising inclined plates of propellant and deflectors, and a propulsion system using a charge of this type
Pyrotechnic charge, with a short combustion time, comprising inclined plates of propellant and deflectors, and a propulsion system using a charge of this type. The pyrotechnic charge is intended...
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4187676 |
Bi-metallic thermal compensator for mounting a solid propellant grain
A rocket assisted projectile is equipped with a bi-metallic disk which ches shape to compensate for propellant grain growth or shrinkage with change in ambient temperature for maintaining the...
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4120153 |
Solid propellant gas generating device
1. In combination with a vessel forming a rocket motor combustion chamber, a rubber-base liner firmly adhering to the interior chamber wall, said rubber-base liner containing between about 2.5 and...
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4118928 |
Means for mounting solid propellant in a rocket motor
A solid propellant grain is held within a rocket motor case in a substantially stress-free manner. The grain is not bonded to the case itself but is bonded to a sleeve which has lateral protrusions...
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4116131 |
Solid propellant motor
A case bonded end burning solid propellant rocket motor utilizing a propellant having sufficiently low modulus to avoid chamber buckling on cooling from cure and sufficiently high elongation to...
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4085584 |
Barrier system for dual-pulse rocket motor
A barrier system for use in preventing the pre-ignition of second pulse rocket grains in a dual pulse rocket motor. The system includes two double layers of rubber material positioned between the...
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3991565 |
Solid propellant with inhibitor layer in rocket motor
A method of inhibiting combustion of some of the surfaces of a solid propellant charge for or in a rocket motor comprising bonding to said surfaces an elastomeric compound resistant to permeation...
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3990369 |
Flexible, highly-adhesive rocket motor case insulation
A rocket motor case liner material that is the reaction product of tung oil ith phenolic resins with an added filler selected from tricalcium phosphate, boric acid, or powdered asbestos. When cured...
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3967444 |
Technique for preventing afterburning of the inert components of solid-propelled rocket motors by using formamidinesulfinic acid in the binder of the inert components
Formamidinesulfinic acid (thiourea dioxide) is employed as an additive to ert motor components of solid-propelled rocket motors to eliminate afterburning which is defined as the combustion of gases...
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3965676 |
Solid rocket motor
1. In combination with a vessel forming a rocket motor combustion chamber, a rubber-base liner having one surface firmly adhering to the chamber, the opposite surface of said rubber-base liner...
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3962865 |
Rocket motor construction
A rocket motor construction wherein a convolutely wound propellent strip forms a fuel grain disposed within the rocket motor casing. The fuel grain consists essentially of double base propellent...
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3961476 |
Metal interlayer adhesive technique
A rocket motor is described in which a thin layer of metallic foil or the ke is used between a silicone rubber insulator and an isocyanate cured, hydroxy terminated polybutadiene bound propellant...
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3961581 |
Ignitor element for a generator of hot gas
The igniter of the generator is constituted by a deformable plate of solid ropergol bound and fixed on a wooden or metal sleeve mandrel. The plate has open striae parallel to the axis of the...
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3958417 |
Suppression of unstable burning in rocket motors
A method of suppressing unstable burning in a solid propellant rocket motor comprising combusting a silicone elastomer with burning of the solid propellant to produce a continuous stream of small...
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3952506 |
Rocket motor construction
A solid propellant grain for a rocket is encased in and bonded to an elastomeric insulation sheath. Stresses that would occur between the propellant grain and the rocket case as a result of...
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3947523 |
Composition comprising epoxy resin, copolymer of butadiene and acrylic acid, curing agent and inorganic metal salt
1. A composition of matter comprised of an epoxy resin, a copolymer of butadiene and acrylic acid, a curing agent, and between about 2.5 and about 30 percent by weight of an inorganic metal salt...
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3943856 |
Hot gas generators, powder charges therefor, and process of production thereof
In a hot gas generator with lamellar powder charge, the charge comprises a plurality of powder lamellae disposed side by side at regularly spaced intervals and projecting from a flexible shoe in...
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3931765 |
Solid propellant designed to burn centripetally and its use in rocket engines or other motors
A solid cylindrical centripetally burning propellant element having an instantaneous combustion surface of substantially constant magnitude exhibits rotational symmetry of order n (2 ≤ n ≤ 15)...
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3931709 |
Method of loading a solid fuel rocket engine
One or both ends of the body of a solid fuel rocket engine is provided with an internally thickened portion, which serves for the mechanical attachment of additional parts, that is the rocket head...
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3928965 |
Rocket motor construction
A solid propellant grain for a rocket is encased in and bonded to an elastomeric insulation sheath. Stresses that would otherwise occur between the propellant grain and the rocket case as a result...
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3919841 |
Rocket motor apparatus
A plurality of perforated tubes are placed longitudinally between the instor layer and silicone rubber layer of a stress relieving rocket motor liner to insure proper pressure distribution within...
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3916618 |
Holding device for holding a propellant grain in a combustion chamber
A holding device for holding a propellant grain in a combustion chamber, comprising a holder fixed to the top of the combustion chamber by a screw and nut, a supporter-buffer in which the holder is...
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3898934 |
Multistrand powder charge
A multistrand powder charge consists of a bundle of powder strands fixed by one of their ends on a support. The charge is characterized in that there is provision, in the very heart of the bundle...
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3889463 |
Stress relieving liner
A stress relieving rocket motor liner is disclosed. The liner comprises an nsulator layer joined to an inhibitor layer by means of columns extending through perforations in a release layer and a...
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3849983 |
PROPELLANT LINER FOR ACTIVE COOLING
This invention is directed to a device for actively cooling the propellant grain of a missile during captive or free flight when aerodynamic heating conditions are present. The device consists of a...
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3812785 |
PROPELLANT FORMED CURE-SHRINKABLE PROPELLANT MATERIAL
This patent describes a novel caseless ammunition comprising a solid unitary propellant grain of generally uniform circular cross-section and containing a plurality of longitudinal openings therein...
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3807171 |
SUPPORTED HIGH-SURFACE-AREA PROPELLANT CHARGES FOR HIGH-ACCELERATION ROCKETS
A high-acceleration rocket motor in which the propellant is bonded to supting structure in a thin and substantially uniform layer to enable the propellant to withstand high acceleration forces....
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3795106 |
BAFFLED SOLID PROPELLANT MOTOR
One or more baffle plates are positioned along the axial length of a solid propellant motor, positioned in a direction transverse to the axis of the motor. Each disc has an aperture therein so that...
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3786633 |
PROPELLANT IMMOBILIZER AND RESONANCE SUPPRESSION SYSTEM
A system for immobilizing solid propellant grain while providing an impro mechanical suppression of resonant burning comprises a small diameter, tension spring extending within the center bore of...
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3763787 |
CARPET ROLL REINFORCED PROPELLANT AND METHOD FOR MAKING
A composite or modified double base propellant that is reinforced with a substrate material and suspended in a rocket motor case from the head end of the propellant by bonding the propellant to the...
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3760731 |
INFANTRY PROJECTILE
A supersonic high explosive anti-tank projectile capable of being launched from a tube by individual personnel including, at its forward end, stand-off means joined to a generally conical high...
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3756025 |
HANDLING MEANS FOR SLOT FORMERS
In slot formers for solid propellant rocket grains, of the type wherein a disk of propellant is equipped with ribs on one side to provide a radially extending slot between forward and aft...
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3731628 |
GRAIN SUPPORT FOR SOLID PROPELLANT ROCKET MOTOR
A solid propellant rocket motor having a plurality of propellant sheets sorted in a manner that the sheets can be burned from both sides without blowing the propellant sheets out of the nozzle at...
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3726090 |
SUPPORT AND PRESSURE SEALANT FOR CARPET ROLL TYPE SOLID PROPELLANT GRAIN
A rocket motor that has a cartridge type propellant with a foam material ut the propellant grain to support the propellant grain and provide a pressure sealant until the propellant grain has been...
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3724219 |
COMBINATION CATALYTIC REACTOR AND EXHAUST SILENCER FOR INTERNAL COMBUSTION ENGINES
A perforated horizontal partition extends all across a horizontally extended chamber, dividing it into an upper compartment filled with particulate catalytic material and a lower compartment across...
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3713395 |
SOLID PROPELLANT
The propellant grain of a rocket motor is improved by providing flame resant adhesive strips longitudinally on the outer periphery of the grain for centering the grain in the motor case and to...
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3698321 |
ROCKET ASSISTED PROJECTILE
An improved projectile suitable for use in artillery pieces, through preferably in the higher calibres, is disclosed wherein projectile range upon launching by the gun is considerably extended by...
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3690101 |
GROUND FOR FIBERGLASS SOLID ROCKET MOTOR CASE
Means for grounding an electrostatic charge from within a fiberglass case of a solid propellant rocket motor are provided. The rocket motor utilizes a solid propellant grain within a fiberglass...
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3672170 |
PROPELLANT GRAIN SUSPENSION SYSTEM
A stress-free propellant grain suspension system wherein the propellant grain is suspended in the motor casing by means of a viscous liquid and the plenum gas pressure.
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3664133 |
SUPPORTED GRAIN DESIGN FOR HIGH ACCELERATION ROCKET MOTORS
1. A solid propellant rocket motor comprising a case having a generally cylindrical chamber section, a forward closure, and a nozzle section; For carrying solid propellant grain, a plurality of...
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3628457 |
ROCKET-ASSISTED PROJECTILE OR GUN-BOOSTED ROCKET WITH SUPPORTED PROPELLANT GRAIN
A rocket-assisted projectile having a central supporting tube surrounded by an annular propellant charge, with an annular space between the tube and propellant decreasing in width towards the rear...
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3600895 |
MEANS FOR LOCATING A CYLINDRICAL PART IN AN AXIAL POSITION IN A HOLLOW CYLINDRICAL PART, MORE ESPECIALLY FOR A PROPELLANT CHARGE BODY AND A JET NOZZLE
Means for locating a cylindrical part in an axial position in a hollow cylindrical part such as a propellant charge body and a jet nozzle body. A split spring washer grips in a circular groove in...
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