FIELD: transport.
SUBSTANCE: invention relates to transportation of rockets by carriers. Proposed device comprises airtight surface on the sides of said support and rocket, are rarefaction system, pipelines, distribution system, pressure gage and suction cups with seal. Damping pad with suction cups is laid between two uneven mating surfaces. Chamber of suction cups are divided by flexible membrane into two chambers, each including individual channel with valve. Said valve is designed to communicate with or disconnect from preliminary or constant rarefaction pressure main line.
EFFECT: simple and reliable design.
4 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROCKET FASTENING AT CARRIER SUPPORT WITH HELP OF SHOCK-ABSORBING PAD WITH SUCTION CUPS | 2012 |
|
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SU1712217A1 |
