REDUCTION OF FALL AREA FOR CARRIER ROCKET FIRST-STAGE UNITS IN CASE OF THEIR PARALLEL COUPLING Russian patent published in 2015 - IPC B64G1/62 

Abstract RU 2572014 C1

FIELD: aircraft engineering.

SUBSTANCE: rocket first-stage units are equipped with the flexible rope-type mechanical linkage. Said rocket units are detached from the carrier rocket second stage to launch the parachute system. The rocket units are stabilized to suppress their hypersonic speeds. The rocket units are descended with the help of space parachute system to surface them at the fall area.

EFFECT: reduced distance between fall area and launching site and fall area proper.

4 dwg

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RU 2 572 014 C1

Authors

Mekhonoshin Jurij Gennad'Evich

Chizhukhin Vladimir Nikolaevich

Dates

2015-12-27Published

2014-05-28Filed