FIELD: transport.
SUBSTANCE: invention relates primarily to aerospace engineering and can be used for launching payloads into orbit. Proposed system comprises mother aircraft, carrier rocket and payload secured in onboard heatproof carrier-launcher container furnished with separation device to allow carrier rocket to detach from mother aircraft. Each tank of the rocket is enclosed in a jacket with its material selected so that to form a stable protective gas bubble around the tank on releasing transpirations from the tank inside its jacket.
EFFECT: decrease in rocket carrier fuel losses.
2 cl
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