METHOD OF PLACING CLUSTER SPACE ROCKET IN ORBIT AT FLIGHT LEG BEFORE SEPARATION OF SIDE BLOCKS Russian patent published in 2013 - IPC B64G1/00 

Abstract RU 2481247 C1

FIELD: transport.

SUBSTANCE: invention relates to aerospace engineering and may be used in clustered rocket bodies. At flight leg before separation of side blocks, program banked turn to appropriate attachment azimuth is performed to align initial angle for registration of appropriate planes with preset attachment azimuth. Pitch is varied to preset program for separation of used side blocks. In injecting the rocket with appropriate planes making angles of 45 degrees with mirror planes, banked turn is performed in two steps, i.e. in 5-10 sec after launching banked turn through 45 degrees is performed and, after pitch angle reaches maximum tolerable magnitude with due allowance for constrictions of gyrostabilised platform kinematics, rocket is turned through 45 degrees to align it with appropriate plane with preset attachment azimuth.

EFFECT: unified control hardware.

6 dwg

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RU 2 481 247 C1

Authors

Al'Tshuler Aleksandr Sholomovich

Volodin Valerij Dmitrievich

Lobanov Vladimir Anatol'Evich

Dates

2013-05-10Published

2011-12-27Filed