UNIVERSAL SYSTEM FOR SAVING spacecraft launch, operate the engine upper stage

摘要

The invention relates to a rescue system space engineering and is intended to save space for various purposes at the start (both manned and unmanned - freight) in case of emergency situations. The technical result of the claimed invention is that the need for the stated minimum SAS launch vehicle retrofitted without requiring radical changes in technology; CAC has better aerodynamics; SAS does not increase the weight of the rocket; there is the possibility of salvation, not only people, but also the goods, ie use SAS for safety launches unmanned vehicles. Said technical result is achieved due to the fact that the emergency rescue system consisting of motors, pyrotechnic separation system is catapulted from the rocket booster module and a parachute landing system, characterized in that the engine system used motors of the rocket booster head unit. Preferably, the catapult system is arranged on the base unit, consisting of several shafts, each of which has a cutter with EB, wherein each barrel laid dampers having a softening function of the dynamic force when the squib; Pyrocartridges consist of a material that provides a relatively smooth gradual detonation; synchronizing all trunks connected annular gas passage, the pressure in the equalizing shafts; in trunks inserted rods attached to a detachable stage.