FIELD: engines and pumps.
SUBSTANCE: invention may be used in detached rocket engines (DRE). A DRE braking device comprises a parachute in a container in the form of a thin-walled pipe with a plug, a pyromoderator, a powder sample, a rope to connect the DRE and the piston with parachute slings, a unit of parachute fixation in the form of a cut element, a case.
EFFECT: invention makes it possible to reduce structure weight and to increase reliability of a DRE braking device.
2 cl, 7 dwg
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