Position control system of a missile during flight under missile Project MX770 are explained. An auto pilot controls the flight through Reads Electronic Analog Computer or REAC. Disturbances like wind, dust or engine failure are evaluated from flight equation. The auto pilot control the path of the flight through hydraulic server. Generally the movable control system is mounted on hinges of a plane as shown in the TL-238. The rotatory equator moves the control system and positions the flight correctly.
Schematic diagram of rocket motor power plant of RTV-A-5 and Navaho 2 missiles is given. Various parts of the motor are shown and their position is specified. Animation shows pathway of fuel to combustion chamber. Vertical and horizontal view of rocket in test stand is given. Day and night view of rocket fired from Santa Susanna field are shown.
Vertical view of operation stand is shown. A gantry crane transfers rocket from operation stand to (73000 lb thrust) static test stand. Technicians control rocket through automatic sequencing and firing panel from the control block house. As the rocket is fired, thrust impact and smoke are seen. Technicians are visualizing and controlling the rocket . A diagram of rocket motor and animation of fuel path is also given.
First flight of the XSM-64 Five Flight Program is shown. XSM-64 ready for launch stands vertically on the launch-stand. The missile is fired and it shoots-up. As the missile moves, it's path is first vertical, then it bends and finally it over turns downwards, making a parabola. Clear trail of fire at tail end of the missile as the missile is fired. Engine ejects as missile approaches earth.
Test fire of Navaho missile XSM-64 under the XSM-64 Five Flight Program is shown. XSM-64 stands vertically on the launch-stand. The missile is fired. Thrust of the missile on the stand shakes it. As the missile moves, it's parabolic path is visualized. Clear trail of fire at tail end of the missile is seen as the missile is fired. Engine is ejected as missile approaches earth.
XSM-64 stands vertically on the launch-stand. The missile uses two chambered liquid fuel engine. As the missile is test-fired thrust of the missile shakes the stand. The missile moves in parabolic path. A trail of fire at tail end of the missile is seen as the missile is fired. Engine ejects as missile approaches downwards.
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