USA As Represented by Secretary of the Navy

US Government As Represented by the Secretary of the Army

Paul E Anderson

Michael D Haddon

Victor Stepanov

Hongwei Qiu

Alex Paraskos

An electronic thermally-initiated venting system (ETIVS) for rocket motors includes at least one linear-shaped charge attached to a rocket motor housing. At least one exploding foil initiator (EFI) is attached to the linear-shaped charge. At least one electronic thermally-initiated venting system circuit is electrically-connected to the EFI. The EFI is configured to auto-fire when the electronic thermally-initiated venting system circuit relays a current pulse through the EFI. The linear-shaped charge is configured to initiate when the current pulse is relayed through the EFI.

Electronic thermally-initiated venting system (ETIVS) for rocket motors

A method of selectively increasing the sensitivity of an insensitive munition by inducing porosity or Joule heating in munitions assembly comprising a power source, an explosive apparatus and a fuze apparatus wherein the explosive apparatus contains a sensitized main explosive composition comprising a secondary explosive and a sensitizing agent. As a result, the otherwise insensitive munition is rendered sensitive to a propagating wave shock by approximately 10 to 25%. To this end, a voltage is applied across the main conductive explosive composition within the insensitive munition. Voltages above certain thresholds cause the decomposition of the explosive material or conductive binder, which leads to an increase in porosity, and therefore the shock sensitivity.

Voltage induced porosity in insensitive munition

Embodiments relate to fuze setback validation. An electronic setback validator for a launched munition safe-arm fuze includes a transient voltage suppressor. A piezoceramic element is electrically-connected to the transient voltage suppressor. A first electronic circuit is electrically-connected to the piezoceramic element and is a constant 1 milliamp discharge circuit. The first electronic circuit is configured to determine setback magnitude of acceleration. A second electronic circuit is electrically-connected to the piezoceramic element. The second electronic circuit is a constant 122 microamp charge circuit and is configured to determine setback duration of acceleration. A microcontroller is electrically-connected to the first and second electronic circuits.

Electronic setback validation for fuzes

An insensitive crystalline high explosive molding powder, usable as a booster HE. The subject insensitive crystalline high explosive molding powder being manufactured by adding the crystalline high explosive, metal or semi-metal particles and a polymer or wax based binder to a solvent to form a solution, spray drying the solution to drive off the solvent, thereby co-precipitating the HE and binder to form granules in which the crystals of HE and metal particles are uniformly distributed in the binder.

Spray drying of metallized explosive

A method of in-situ remediation of chlorinated and fluorinated reaction by-products resulting from energetic detonations and/or burning of energetic mixtures comprising adding a quantity of Calcium disilicide (CaSi), Calcium silicide (CaSi), Magnesium disilicide (MgSi), Magnesium silicide, or Aluminum Calcium (AlCa) compounds to the energetic mixture prior to its detonation and/or burning. Advantageously, the in-situ production of more inert by-products results from this addition thereby preventing the formation of any less-desirable by-products.

Growing community of inventors

Ridgecrest, CA, United States of America

Paul E Anderson