Invention Grant
- Patent Title: Thermally initiated variable venting system for rocket motor
-
Application No.: US16136125Application Date: 2018-09-19
-
Publication No.: US10830181B2Publication Date: 2020-11-10
- Inventor: Luis G. Interiano
- Applicant: GOODRICH CORPORATION
- Applicant Address: US NC Charlotte
- Assignee: Goodrich Corporation
- Current Assignee: Goodrich Corporation
- Current Assignee Address: US NC Charlotte
- Agency: Snell & Wilmer L.L.P.
- Main IPC: F02K9/38
- IPC: F02K9/38 ; B64G1/40 ; F42B39/20 ; F02K9/92 ; F02K9/26 ; F42B39/14 ; F02K9/08 ; F02K9/95
Abstract:
A thermally initiated variable venting system may comprise a first linear shape charge (LSC) coupled to a first sensor and a second LSC coupled to a second sensor. An upper apex of the second LSC may be disposed within a lower apex of the first LSC. The output of the system may vary depending on whether the event is fast cook-off (FCO) or slow cook-off (SCO).
Public/Granted literature
- US20200088137A1 THERMALLY INTITIATED VARIABLE VENTING SYSTEM Public/Granted day:2020-03-19
Information query
