| 摘要 |
The method involves setting unmanned missile (2) at a joggle aperture (12) of aircraft (1). A braking parachute (3) is secured at brake line (30) provided at rear of missile. A carrying parachute (4) is fixed by front support line (42) and rear support line (44) provided at the top of the missile. The braking parachute is released from missile. The front support line of carrying parachute is disconnected so that front end of missile acquires pitch movement downwardly out.The rear support line of carrying parachute is disconnected so that flight structure of missile merges into free flight. |
