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Program of High Mach Integrated Control Experiment, “HIMICO” Using S-520 Sounding Rocket.

Authors :
Tetsuya SATO
Hideyuki TAGUCHI
Takayuki KOJIMA
Takeshi TSUCHIYA
Mitsuhiro TSUE
Shinji NAKAYA
Akiko MATSUO
Asei TEZUKA
Takahiro FUJIKAWA
Koji MIYAJI
Source :
Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan; 2021, Vol. 19 Issue 6, p831-837, 7p
Publication Year :
2021

Abstract

JAXA and some universities have proposed a hypersonic flight experiment named “HIMICO: High Mach Integrated Control Experiment” using a 1.5-meter class vehicle launched by the S-520 sounding rocket. The experiment aims to establish an integrated control method including the interference between the airframe and engine under the actual Mach 5 flight condition. Two flight experiments are planned step by step to reduce technical risks. Feasibility studies have been conducted by experiments and CFD analysis. This paper reports the summary of the flight test plan and preliminary studies on the vehicle shape, flight trajectory, component design and technical issues. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
18840485
Volume :
19
Issue :
6
Database :
Complementary Index
Journal :
Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan
Publication Type :
Academic Journal
Accession number :
153463012
Full Text :
https://doi.org/10.2322/tastj.19.831