The invention relates to a method and an arrangement for controlling the range of a projectile propelled by a rocket motor. An actual value of a quantity clearly correlating with the distance covered by the projectile is continuously determined during the ...

A rocket nozzle assembly is provided for operatively coupling to a rocket motor. The assembly includes a nozzle insert structure having a converging-diverging passageway with a throat region. First and second thrust control cylinders are parallel to each o...