FIELD: applicable for protection against ballistic missiles. SUBSTANCE: it is recommended to use an intercepter missile launched from a glider delivered to the design point by flying vehicles. Launching is accomplished at the maximum altitude and speed on a curved trajectory, whose downward leg is matched with the trajectory of the ballistic missile. After the above trajectories are matched, a parachute is released from the intercepter missile for its engagement with the ballistic missile. EFFECT: enhanced probability of destruction. 3 cl
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR DESTRUCTION OF BALLISTIC MISSILE | 1999 |
|
RU2162589C1 |
METHOD OF AIR OBJECTS HITTING | 2017 |
|
RU2651407C1 |
METHOD OF CONTROL OF HIGH-SPEED FLYING OBJECT IN ZONE OF DANGER OF DESTRUCTION | 1999 |
|
RU2158697C1 |
METHOD OF INJECTION OF ROCKET INTO NEAR-EARTH ORBIT | 1997 |
|
RU2131831C1 |
METHOD OF DESTRUCTION OF COMBAT SURFACE SHIP | 1999 |
|
RU2160212C1 |
METHOD OF REDUCTION OF MINIMUM ALTITUDE OF DESCENT OF OBJECT FROM FLYING VEHICLE | 1997 |
|
RU2120887C1 |
METHOD OF RESCUE OF HELICOPTER | 1997 |
|
RU2130872C1 |
METHOD OF RESCUE OF FLYING VEHICLE IN CASE OF ACCIDENT NEAR LANDING SURFACE | 1997 |
|
RU2130875C1 |
DEVICE FOR RECOVERY OF HELICOPTER | 1997 |
|
RU2128602C1 |
METHOD OF RESCUE OF HELICOPTER | 1997 |
|
RU2130873C1 |
Authors
Dates
2000-08-27—Published
1999-08-10—Filed