Title:
CONTINUOUS IGNITION STRUCTURE OF ROCKET
Document Type and Number:
WIPO Patent Application WO/2019/098473
Kind Code:
A1
Abstract:
The present invention relates to a partial structure of a rocket, which includes a satellite launcher engine and an auxiliary engine added thereto, to enable continuous ignition by a spark method, and more specifically, proposes a continuous ignition structure for a rocket. In other words, the present invention improves a previous technology for a conventional launcher engine, which fails to satisfy an expected propulsive force due to degradation of an engine performance and thus makes a launch failure.
Inventors:
DONG BING JI (KR)
Application Number:
PCT/KR2018/005653
Publication Date:
May 23, 2019
Filing Date:
May 17, 2018
Export Citation:
Assignee:
DONG BING JI (KR)
International Classes:
F02K9/94; F02K9/60; F02K9/95
Foreign References:
KR20040009471A | 2004-01-31 | |||
US9650997B2 | 2017-05-16 | |||
JPH0633834A | 1994-02-08 | |||
KR101279722B1 | 2013-06-27 | |||
KR100582979B1 | 2006-05-24 |
Attorney, Agent or Firm:
PARK, Yochang (KR)
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