Invention Grant
- Patent Title: Dual stage catalytic thruster
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Application No.: US15580051Application Date: 2015-06-30
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Publication No.: US11236703B2Publication Date: 2022-02-01
- Inventor: Matthew Dawson , Gerald Brewster
- Applicant: Aerojet Rocketdyne, Inc.
- Applicant Address: US CA Sacramento
- Assignee: Aerojet Rocketdyne, Inc.
- Current Assignee: Aerojet Rocketdyne, Inc.
- Current Assignee Address: US CA Sacramento
- International Application: PCT/US2015/038505 WO 20150630
- International Announcement: WO2017/003447 WO 20170105
- Main IPC: F02K9/52
- IPC: F02K9/52 ; F02K9/68 ; B64G1/40 ; F02K9/58 ; F02K9/94 ; F02K9/97
Abstract:
A catalytic thruster includes a reaction chamber that extends between first and second opposed chamber ends. The first chamber end includes a thermal standoff cup. There is a catalyst bed in the reaction chamber, and a feed tube extends into the reaction chamber through the thermal standoff cup.
Public/Granted literature
- US20180135559A1 DUAL STAGE CATALYTIC THRUSTER Public/Granted day:2018-05-17
Information query
