METHOD FOR SEPARATING A SPACE VEHICLES GROUP FROM A ROCKET-CARRIER AND A DEVICE FOR ITS IMPLEMENTATION

摘要

FIELD: rocketry.SUBSTANCE: group of inventions relates to aerospace engineering. In the method of separation from the carrier rocket (CR) the 4 spacecraft groups (SC) 7, in case of non-separation one SC 7, the next SC 7 is separated, after the command for separation is given of non-separated SC 7 using pyrotechnic device 13, that provides the separation of the SC 7 together with the part of housing 8 of separation system 6 that has collapsed when pyrotechnic device 13 is activated, while simultaneously giving them speed relative to adapter 1. Signal registration of the separation of the SC 7 is carried out by sensors 15 installed on housing 8 of separation system 6. Device for implementing of the method comprises adapter 1 consisting of base 2 with attachment points 3 to carrier rocket 4 and platform 5 connected to base 2, separation system 6 of SC 7 fixed to platform 5. Closed channels 12 with pyrotechnic devices 13 are made, for example, in the form of low-pulse detonating cords, on the outer perimeter of shells 8. Pyrotechnic devices 13 are closed with protective covers 14.EFFECT: technical result of the group of inventions is to increase the reliability of separation of SC from CR.2 cl, 6 dwg