FIELD: machine building.
SUBSTANCE: rocket launcher comprises a flow-through launch tube with a nozzle connected by an opening to the outlet (in the form of a control injection valve or a supersonic nozzle) of the secondary mass carrier.
EFFECT: invention provides for the adjustment of compensating gas dynamic force for a launcher at rocket start.
3 cl, 2 dwg
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|
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|
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| MISSILE LAUNCHING PLANT | 2014 |
|
RU2545154C1 |
