FIELD: submarine rocketry. SUBSTANCE: simultaneously with removal of rigid coupling between the rocket and shock-absorbers solid-propellant gas generator gets actuated, whose gases pressurize two flattened tubular elements, thus transforming the shock-absorbing belt into a ring of a larger diameter. After that the shock-absorbing belt comes off the rocket under the action of the air velocity flow and the thrust of the rocket engine installation. EFFECT: reduced quantity of objects falling on the submarine, improved conditions of shockless motion of rockets at salvo fire. 3 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SHOCK-ABSORBING DEVICE OF NAVAL BALLISTIC MISSILE | 2001 |
|
RU2199082C1 |
| RUBBER-METAL SHOCK ABSORBER | 2000 |
|
RU2181455C2 |
| TECHNIQUE AND GEAR TO STABILIZE MOTION OF SEA BALLISTIC MISSILE OVER UNDERWATER RUN | 2000 |
|
RU2193155C2 |
| METHOD OF EVACUATION OF CREW FROM EMERGENCY SUBMARINE AND DEVICE FOR REALIZATION OF THIS METHOD | 1997 |
|
RU2149123C1 |
| METHOD TO START A ROCKET FROM A SHAFT OF A SUBMARINE | 2002 |
|
RU2235286C2 |
| METHOD FOR MANUFACTURE OF RUBBER SHOCK MOUNTING | 2003 |
|
RU2261380C2 |
| DEVICE FOR SEPARATION OF STAGES OF A MARINE-BASED LIQUID FUEL BALLISTIC MISSILE | 2002 |
|
RU2235287C2 |
| DESCENT SPACECRAFT | 2002 |
|
RU2234442C2 |
| SHIPBORNE CONTAINER FOR ROCKET STORAGE AND LAUNCH | 2000 |
|
RU2194235C2 |
| METHOD AND DEVICE FOR GUIDED MISSILE TAKE-OFF FROM TRANSPORT-LAUNCHING PACK | 2003 |
|
RU2240489C1 |
