Journal of the Combustion Society of Japan
Online ISSN : 2424-1687
Print ISSN : 1347-1864
ISSN-L : 1347-1864
FEATURE —A Story of the "Beautiful Flame"
A Story of "World First! Detonation Engine Space Demonstration"
Jiro KASAHARAKoichi MATSUYAMAKen MATSUOKAAkira KAWASAKIHiroaki WATANABENoboru ITOUYAMAKeisuke GOTOKazuki ISHIHARAValentin BUYAKOFUTomoyuki NODAAkiko MATSUOIkkoh FUNAKIHiroto HABUShinsuke TAKEUCHISatoshi ARAKAWAJunichi MASUDAKenji MAEHARAKazuhiko YAMADATatsuro NAKAOShuichi NAKAMURAShinji TOYONAGAOsamu HARADAHidefumi KAWANOFumitaka YAMAMOTOSyouji KAWAMOTOKazuyuki HIGASHINODaisuke NAKATAMasaharu UCHIUMINaoya MITAHiromi JINDOIchiro DOYAMATatsuya KATOSounding Rocket S-520-31 Experiment Team
Author information
JOURNAL RESTRICTED ACCESS

2023 Volume 65 Issue 214 Pages 220-223

Details
Abstract

A detonation engine in space flight has been successfully demonstrated. This is the world's first successful demonstration of a detonation engine in space. The detonation engine system developed in this study was loaded onto the mission section of the sounding rocket S-520-31 and launched from the JAXA Uchinoura Space Center at 5:30 a.m. on July 27, 2021. After the separation of the first stage rocket, the rotating detonation engine and pulse detonation engine were successfully operated in space, and photo images, pressure, temperature, vibration, position, and attitude data were acquired by telemetry and RATS (Reentry and Recovery Module with Deployable Aeroshell Technology for Sounding Rocket Experiment). The fuel is methane and the oxidizer is oxygen. The detonation engine generates detonation and compression waves at extremely high frequencies (1-100 kHz) to drastically increase reaction speed, leading to radical reduction of rocket engine weights and high performance by easy generation of thrust. The success of this space flight demonstration will bring the detonation engine much closer to practical use as a kick motor for deep space exploration, and as a first and second stage engine for rockets.

Content from these authors
© 2023 Combustion Society of Japan
Previous article Next article
feedback
Top