Invention Grant
- Patent Title: Hypergolic hybrid motor igniter
- Patent Title (中): 超音速混合动力点火器
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Application No.: US13434223Application Date: 2012-03-29
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Publication No.: US09273635B2Publication Date: 2016-03-01
- Inventor: Brian Blaise Brady , John D DeSain
- Applicant: Brian Blaise Brady , John D DeSain
- Applicant Address: US CA El Segundo
- Assignee: The Aerospace Corporation
- Current Assignee: The Aerospace Corporation
- Current Assignee Address: US CA El Segundo
- Agency: Leonard Patel PC
- Main IPC: F02K9/72
- IPC: F02K9/72

Abstract:
An apparatus for igniting a larger rocket motor is provided. The apparatus may be a smaller rocket motor that can be ignited hypergolically, when a pressurized oxidizer contacts hypergolic fuel grains of the smaller rocket motor. The hypergolic ignition causes the larger rocket motor to be ignited. The hypergolic ignition of the smaller rocket motor may be stopped after the larger rocket motor is ignited, and the remaining hypergolic fuel grains and the pressurized oxidizer can be reserved for reigniting the larger rocket motor at a later time.
Public/Granted literature
- US20130255223A1 HYPERGOLIC HYBRID MOTOR IGNITER Public/Granted day:2013-10-03
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