Proj
J-GLOBAL ID:200904027345557550  Research Project code:0350012070 Update date:Jan. 19, 2004

Research on aerodynamics of VTOL rocket

垂直離着陸型ロケットの空力に関する研究
Study period:2001 - 2001
Organization (1):
Investigating Researcher (3):
Research overview:
VTOL rocket, capable of eliminating wings, is superior to a winged flying object in structural weight, and has an advantage that the body shape is not limited by the wings. On the other hand, aerodynamic limitations exist in a smaller lift in comparison with a winged structure and limited guidability. Technical issues to be solved for system construction are reviewed on the aerodynamics of VTOL rocket.
Research program: Ordinary Research
Ministry with control over the research :
Ministry of Education, Culture, Sports, Science and Technology

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