Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
Innovative Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Jet Engine Technology Research Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Unmanned Aircraft Systems Applications Technology Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)
Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
Unmanned Aircraft Systems Applications Technology Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)
Department of Spacecraft Engineering, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
Flight test of Balloon Based Operation Vehicle (BOV) was conducted to demonstrate key technologies for future hypersonic transport and space planes. Main objective of the flight test was to demonstrate hypersonic turbojet engine under Mach 2 flight condition. The vehicle runs on gaseous hydrogen and liquid nitrogen. This paper describes system vehicle system including such flammable gas and high pressure gas and operating system of them.
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
気球利用型実験機(BOV3号機)の地上作業
65489000.pdf
(2.96MB)
