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|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/31 ; 244/324 ; 102/529|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 13 인용 특허 : 8|
A spin-stabilized training missile is equipped with a stabilizer device for reducing spinning in order to decrease the flight range. The training missile is designed so that its stabilization attainable solely by the spin upon firing is not sufficient for a stable flight in the practice range. The required additional stabilizing in the practice range is obtained by a stabilizer device or control airfoil effecting simultaneously, after leaving the practice range, such a spin reduction that the training missile becomes unstable and the range of flight is c...
A spin-stabilized training missile which comprises a base member shaped as a missile with a stabilizer means for reducing spin in order to decrease the flight range, the base member of the training missile, upon firing, having a stability due to spin that is too low for stable flight, and said stabilizer means comprises at least one element having a stabilizer surface which effects, on the one hand, an additional aerodynamic stabilization providing stable flight in the training range together with the spin stabilization of te base member and, on the othe...