| 摘要 |
FIELD: weapons. ^ SUBSTANCE: invention concerns missile technology, particularly multistage missile construction. Two-stage guided missile includes separable march stage, launching engine with stabiliser unit, and separation device. To improve missile reliability, simplify land controls and prevent launching engine fall outside the zone of enemy troops, weight ratio of march stage and launching engine without fuel should be defined. Invention claims dependency for defining the indicated ratio. ^ EFFECT: improved missile reliability, simplified land controls and prevented fall of launching engine outside the zone of enemy troops. ^ 2 dwg |
