Invention Grant
- Patent Title: Solid rocket motor with vortex inducing feature
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Application No.: US15571270Application Date: 2016-07-26
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Publication No.: US10883448B2Publication Date: 2021-01-05
- Inventor: Samuel Steven Schlueter
- 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/US2016/043982 WO 20160726
- International Announcement: WO2017/027198 WO 20170216
- Main IPC: F02K9/18
- IPC: F02K9/18 ; F02K9/34 ; F02K9/08 ; F02K9/16 ; F02K9/10 ; B64G1/40 ; F02K9/24
Abstract:
A solid rocket motor includes a propellant grain structure defining an axial bore and a vortex inducing feature.
Public/Granted literature
- US20180112627A1 SOLID ROCKET MOTOR WITH VORTEX INDUCING FEATURE Public/Granted day:2018-04-26
Information query
