NASA/SP-8114, NASA SPACE VEHICLE DESIGN CRITERIA (CHEMICAL): SOLID ROCKET THRUST VECTOR CONTROL (DEC-1974)

NASA/SP-8114, NASA SPACE VEHICLE DESIGN CRITERIA (CHEMICAL): SOLID ROCKET THRUST VECTOR CONTROL (DEC-1974)., Thrust vector control systems that superimpose a side force on the motor thrust, steering being achieved by the side force causing a moment about the vehicle center of gravity are described. A brief review of thrust vector control systems is presented, and two systems, flexible joint and liquid injection, are treated in detail. Treatment of the flexible-joint thrust vector control system is limited to the design of the flexible joint and its insulation against hot motor gases. Treatment of the liquid injection thrust vector control system is limited to discussion of the injectant, valves, piping, storage tanks, and pressurization system; no evaluation is presented of the nozzle except for (1) the effect of the injectant and erosion at the injection port and (2) the effect of injection on pressure distribution within the nozzle.