Invention Grant
- Patent Title: Device for pressurizing propellant tanks of a rocket engine
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Application No.: US14909894Application Date: 2014-07-25
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Publication No.: US10533523B2Publication Date: 2020-01-14
- Inventor: Gérard Roz , Lauren Nguyen Duc , Stéphanie Dreyer , Nicolas Ravier
- Applicant: SNECMA
- Applicant Address: FR Paris
- Assignee: ARIANEGROUP SAS
- Current Assignee: ARIANEGROUP SAS
- Current Assignee Address: FR Paris
- Agency: Bookoff McAndrews, PLLC
- Priority: FR1357808 20130806
- International Application: PCT/FR2014/051941 WO 20140725
- International Announcement: WO2015/019000 WO 20150212
- Main IPC: F02K9/50
- IPC: F02K9/50 ; F02K9/94 ; F02K9/97

Abstract:
The device comprises two heat exchangers (74, 90) suitable respectively for vaporizing first and second propellants before they are reintroduced in gaseous form into their tanks (16, 18). The heat exchangers co-operate respectively with first and second gas generators (60, 84) suitable for being fed with a mixture of propellants in order to produce combustion, the second gas generator (84) being suitable for being fed at least in part by the exhaust from the first gas generator (60).
Public/Granted literature
- US20160177874A1 DEVICE FOR PRESSURIZING PROPELLANT TANKS OF A ROCKET ENGINE Public/Granted day:2016-06-23
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