Ensign-bickford Aerospace & Defense Company

Kurt Nelson

Andrew M Kochanek

Joseph Stork Smith

Daniel P Sutula, Jr

Craig Boucher

John A Graham

Scott D Crespi

Scott Gammons

Marc Morris

John Benner

Michael Ronzello

James Danyluk

Jared Holtman

Jarrett Jacobson

Alan Garvey

John Fiske

Matthew Bragoni

Edris Raji

A system that is mountable to an unmanned vehicle and a method of operation is provided. The system includes an attachment plate configured to couple to the unmanned vehicle, the attachment plate having a first feature. A control module is configured to removably couple to the attachment plate, the control module having one or more processors and a power source, the control module having a pin arranged to move from a first position to a second position when the control module is coupled to the attachment plate, the one or more processors being energized when the pin is moved from the first position to the second position. A payload having an energetic element is provided, the payload being coupled to the control module.

Payload platform for unmanned vehicles

A casing segmentation device and system, and a method for selectively providing a fluid flow passage through a casing segmentation device disposed within a well casing segment is provided. The casing segmentation device includes a body and a fracture mechanism. The body has a forward end, an aft end, a plug seat, and an internal passage. The plug seat is configured to receive a mating plug. The internal passage extends between the forward end and the aft end and through the plug seat. The fracture mechanism includes an amount of energetic material and a trigger mechanism. The trigger mechanism is configured to selectively cause a detonation of the amount of energetic material.

Destructible casing segmentation device and method for use

A rocket having a motor with a user adjustable thrust is provided. The rocket includes a main cylinder containing a rocket propellant, the propellant configured to generate gas during operation and one or more nozzles arranged to direct the gas in a first direction. A thrust adjustment device is arranged to receive a portion of the gas, the thrust adjustment device configured to change the direction of flow of at least a portion of the gas.

Rocket motor with means for user adjustable thrust

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West Simsbury, CT, United States of America

Kurt Nelson