发明名称 MONOPROPELLANT INJECTOR FOR SMALL-SIZED THRUSTER
摘要 PURPOSE: A monopropellant injector for a small thruster is provided to supply a monopropellant over a wide range by forming a plurality of discharge ports. CONSTITUTION: A monopropellant injector for a small thruster comprises an injection plate and a plurality of discharge ports(130). The injection plate is mounted to the end of a combustion chamber. The discharge ports inject a monopropellant to the combustion chamber. The discharge ports are formed in the injection plate. A virtual line from one discharge port crosses over another virtual line from the other discharge port. The monopropellant from the discharge ports is atomized by colliding each other in the combustion chamber.
申请公布号 KR20120111631(A) 申请公布日期 2012.10.10
申请号 KR20110030229 申请日期 2011.04.01
申请人 KONKUK UNIVERSITY INDUSTRIAL COOPERATION CORP.;KOREA AEROSPACE RESEARCH INSTITUTE 发明人 BYUN, DO YOUNG;KIM, KI RO;YU, MYOUNG JONG;KIM, SU KYUM
分类号 F02K9/52;B64G1/26;B64G1/40;F02K9/44 主分类号 F02K9/52
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