Select the phrase that best completes the statement.
Thrust control is provided on a liquid fueled rocket by:
- Varying the nozzle size while in flight.
- Controlling the fuel flow to the engine.
- Actuating the reverse thruster pods.
- N/A -- Thrust cannot be controlled on a liquid fueled engine.
You are correct! The answer is B. By controlling the rate of the liquid propellant flow into the combustion chamber, thrust control is achieved.
The correct answer is B. By controlling the rate of the liquid propellant flow into the combustion chamber, thrust control is achieved.
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