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
Title | Year | Author | Number |
---|---|---|---|
METHOD OF AUTONOMOUS NAVIGATION FOR SPACE OBJECT | 2018 |
|
RU2727784C2 |
METHOD OF SAFE LAUNCHING OF ROCKET WITH MULTIENGINE FIRST STAGE | 2011 |
|
RU2481251C1 |
METHOD OF ONBOARD CONTROL IN ROCKET FLIGHT EMERGENT TERMINATION | 2011 |
|
RU2476357C2 |
METHOD OF KILLING ELASTIC VIBRATIONS OF CLUSTERED ROCKET BODY | 2011 |
|
RU2474517C2 |
METHOD OF PROTECTING LAUNCH SITE COMPONENTS AGAINST ROCKET ENGINE JETS GASDYNAMIC EFFECTS | 2009 |
|
RU2407680C1 |
ANTIFAILURE PROTECTION OF ROCKET MULTIPLEX CONTROL SYSTEM | 2012 |
|
RU2521117C1 |
METHOD OF DESCENDING SEPARATED SPACE ROCKET STAGE AND DEVICE THEREFOR | 2015 |
|
RU2581894C1 |
METHOD OF DESCENT OF SPACE ROCKET BOOSTER TO TOUCHDOWN ZONE AND DEVICE FOR ITS REALIZATION | 1992 |
|
RU2043954C1 |
METHOD OF LAUNCHING ROCKET FROM AIRCRAFT TO PLACE PAYLOAD INTO ORBIT | 2008 |
|
RU2394201C2 |
METHOD FOR MISSILE TAKE-OFF FROM AIRCRAFT FOR ORBIT INJECTION OF PAYLOAD | 2004 |
|
RU2289084C2 |
Authors
Dates
2013-05-10—Published
2011-12-27—Filed