Title:
PROPULSION DEVICE FOR LIQUID PROPELLANT ROCKET ENGINE
Document Type and Number:
WIPO Patent Application WO/2020/050689
Kind Code:
A1
Abstract:
Provided is a propulsion device for a liquid propellant rocket engine according to an embodiment, comprising: a main body into which a liquid propellant is introduced; an injector core located inside the main body; at least one outlet connected to the injector core for exhausting combustion gas; and an injector for discharging the liquid propellant introduced into the main body, wherein the injector is located in an area adjacent to the outlet, and the liquid propellant moves between the frame of the main body and the frame of the injector core.
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Inventors:
SHIN DONG YOON (KR)
Application Number:
PCT/KR2019/011562
Publication Date:
March 12, 2020
Filing Date:
September 06, 2019
Export Citation:
Assignee:
PERIGEE AEROSPACE INC (KR)
International Classes:
F02K9/52; F02K9/95
Foreign References:
| US20180112628A1 | 2018-04-26 | |||
| KR101631891B1 | 2016-06-20 | |||
| JP2005061385A | 2005-03-10 | |||
| US20100107601A1 | 2010-05-06 | |||
| US5768885A | 1998-06-23 |
Attorney, Agent or Firm:
IPS PATENT FIRM (KR)
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