The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Apr. 04, 2017

Filed:

Jan. 26, 2015
Applicant:

Sparton Corporation, Schaumburg, IL (US);

Inventors:

David Powell, Sanford, FL (US);

Earl Mark, Deleon Springs, FL (US);

Keith Huber, Palm Coast, FL (US);

Taylor Durrance, Daytona Beach, FL (US);

Tanner Sizemore, Wildwood, FL (US);

Charles M. Nowell, Jr., Longwood, FL (US);

Assignee:

Sparton Corporation, Schaumburg, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F41F 3/07 (2006.01); F41F 3/077 (2006.01);
U.S. Cl.
CPC ...
F41F 3/07 (2013.01); F41F 3/077 (2013.01);
Abstract

A payload launch system includes a launch tube, payload, rocket tube, pressurized motor assembly, and control system. The motor assembly has a launch actuator and an accumulator housing containing compressed gas. The accumulator housing defines a vent opening having a closure. The control system transmits an actuation signal to the actuator in response to a launch request signal to open the closure and cause a discharge of pressure into the launch tube. This causes the rocket tube to launch from the launch tube to a threshold altitude in a single gaseous thrust phase. A method includes deploying a launch system, transmitting a launch actuation signal to the launch actuator via a control system, and opening a closure to allow compressed gas to enter the launch tube, thereby launching the rocket tube from the launch tube to a threshold altitude in the single gaseous thrust phase.


Find Patent Forward Citations

Loading…