FIELD: rocketry. SUBSTANCE: destruction of rockets by launching them in a preset trajectory and destruction in an area that is safe for vital activity of people. Data providing for an excess of permissible deviations of rockets from the preset trajectory at the given moment of time are introduced in the flying mission. As a result of these, deviations the emergency self-destruction system gets actuated and the rocket is destructed. EFFECT: operational destruction of rockets without any design changes with minimum effect on environment. 2 cl, 1 ex
Title | Year | Author | Number |
---|---|---|---|
MISSILE WITH SPATIAL LIMITATION OF FLIGHT TRAJECTORY AND METHOD OF ITS SELF-DESTRUCTION | 2019 |
|
RU2724152C1 |
MISSILE WITH A SPATIAL RESTRICTION OF THE FLIGHT PATH | 2022 |
|
RU2788218C1 |
METHOD OF CONTROLLING ROCKET FLIGHT DURING FLIGHT TESTS | 2013 |
|
RU2549425C1 |
CRUISE MISSILE UNIVERSAL IN SCORE AND ENGAGEMENT METHODS | 2015 |
|
RU2622051C2 |
DEVICE FOR ROCKET SELF-LIQUIDATION | 2007 |
|
RU2343399C1 |
MISSILE SELF-DESTROYING DEVICE | 2006 |
|
RU2316722C1 |
METHOD OF OPERATION OF RECOVERABLE SPACECRAFT | 1994 |
|
RU2128610C1 |
DEVICE FOR SEPARATION OF BALLISTIC MISSILE SECTION | 1994 |
|
RU2128816C1 |
JET CODE CHARGE (VERSIONS) | 2011 |
|
RU2510355C2 |
PROCESS OF LAUNCHING OF ROCKET FROM AIRCRAFT | 1992 |
|
RU2068169C1 |
Authors
Dates
1999-10-10—Published
1998-07-24—Filed