J-GLOBAL ID:200904031075014688  Research Project code:9800036287 Update date:Jan. 19, 2004

Research and development of TVC device for M-V type rocke

Study period:1994 - 2002
Organization (1):
Investigating Researcher (4):
Research overview:
Research and development of attitude-control device (TVC device) of M-V type rocket is continued. More specifically, the 2nd stage TVC system has been developed in that the liquid injection system (LITVC) hitherto employed is replaced by the movable nozzle system (MNTVC) as a part of development for lower cost and higher performance system. In the fiscal 2002, a flight model was manufactured to complete the development toward No.5 rocket to be launched in the fiscal 2003. The actuator for this TVC is a high-output electric linear actuator, and it uses large thermal battery for power supply.
Keywords (8):
launch vehicle ,  attitude control ,  control equipment ,  gas turbine ,  combustion test ,  nozzle ,  proportional valve ,  hydrostatic drive
Research program: Ordinary Research
Ministry with control over the research :
Ministry of Education, Culture, Sports, Science and Technology

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