| 摘要 |
The method of controlling a rocket vehicle in which ramp tabs and vane tabs are used to control pitch, roll and spin and the height is controlled by means of all ramp tabs through limiter means arranged to minimise loss of attitude control. The ramp tabs comprise a series of generally symmetrically spaced tabs mounted on the vehicle to be projectable into the efflux stream, the rotation producing tab vane means being angled so that, when projected into the efflux, spin in either direction about the vehicle longitudinal axis. |
