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Correct Answer : Decrease in stagnation temperature
Explanation : Stagnation temperature for an isentropic process remains constant. Static temperature, static pressure, and specific volume may vary.
Correct Answer : Option (A) : Both assertion and reason are correct
Explaination : Usually solid propellant combustion gases are fuel rich and addition of oxygen into this control flow results in a secondary combustion. It increases both stagnation temperature and pressure of the flow. Because of pressure sensitivity on burning rate, higher stagnation pressure results in a higher mass flow rate, while the increase in stagnation temperature results in an increase in the characteristic velocity of the exit jet.
Correct Answer : Option (D) : Throat Shifting Thrust Modulation
Explanation : In Throat Shifting Thrust Modulation (TSTM), by shifting the throat of the nozzle, thrust is controlled. For modulation of thrust, the jet area is controlled using symmetric injection near the throat.
Correct Answer : Option (B) : Shock Thrust Modulation
Explanation : Shock Thrust Modulation (STM) involves an axisymmetric injection of secondary flow into the diverging section of the supersonic nozzle and the creation of a normal shock by the interaction of oblique shocks. Across a normal shock, a supersonic flow becomes subsonic, thereby reducing exhaust velocity and total thrust. Fluidic Thrust Modulation is divided into STM and TSTM.
