AERIAL LAUNCHING ROCKET AND AERIAL LAUNCHING METHOD

摘要

PROBLEM TO BE SOLVED: To solve the problems of a conventional aerial launching rocket, in which a load applied to a connection structure of a main rocket and a booster rocket easily increases, and that fluttering or the like easily occurs.SOLUTION: An aerial launching rocket R which is loaded on an aircraft F in order to be launched, includes: a main missile MV; rocket motors RM disposed on both sides of the main missile; and connection arm devices A connecting the rocket motors to the main missile in a state that each rocket motor RM is spaced apart from the main missile MV. The connection arm devices A comprise edge aligning mechanisms (1 to 3) for moving the rocket motors RM. The aerial launching rocket R, after detaching from the aircraft F, reduces intervals between the main missile MV and the rocket motors RM. Subsequently, since the rocket motors RM are ignited, a load applied to the connection structure of the main missile MV and the rocket motors RM is reduced, a characteristic frequency is largely secured, and fluttering or the like is suppressed.SELECTED DRAWING: Figure 4