US Patent 9612085 Payload launch system and method
Patent 9612085 was granted and assigned to Sparton (company) on April, 2017 by the United States Patent and Trademark Office.
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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.
US Patent 09612085 Payload launch system and method US Patent 9612085 Payload launch system and method
US Patent 09612085 Payload launch system and method
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