국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	A Shock Tunnel Experiment on Aerodynamic Interference Induced by RCS Jet
저자	Takashi YAMAZAKI, Kunio SOGA, Hiroshi WAKAI, Tadashi ISHIKAWA, Kouhei TANAKA
Keyword	Spaceplane; Reaction Control System; Hypersonic flow; Interference
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr01219.pdf?id=NALTR0001219
보고서번호	NAL TR-1219
발행년도	1993.12
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	During the re-entry of a spaceplane,it is necessary to use a reaction control system(RCS) for attitude control augmentation in flight regions where the control surfaces are not fully effective.A shock tunnel experiment was perform