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Rocket Propulsion Practice Test: Flight Performance
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Flight Performance topics include: Gravity free drag free space flight performance, vehicle forces in the atmosphere, motion basic relations, vehicles propulsion system effect, space flight, exhaust plumes aerodynamic effect, flight stability, flight performance on military missiles, flight maneuver and vehicles. The fundamental measure of rocket engine performance is the mass of propellant that can be propelled out the back of the rocket and at what speeds. The performance of a rocket engine depends on the thrust, which is generated relative to the size or weight of the propulsive... Show more
Rocket Propulsion Practice Test: Flight Performance
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25 Questions

1. Suppose an aircraft trimmed at a 10° angle of attack faces a gust that changes the angle of attack to 15°. What is the nature of the moment required to bring it back to the trimmed condition?
2. Station keeping maneuvers are ___________
3. What is the thrust required for a truly rotational maneuver?
4. Which of the following is the mixing layer of a nozzle core flow?
5. What is the angle of attack for a missile?
6. If the velocity increments of the first, second, and third stages are 1000 m/s, 500 m/s and 250 m/s respectively, determine the total velocity increment.
7. The lift and drag coefficients are not primarily a function of ____________
8. Determine the component of gravitational force in the direction of the flight path if the angle of the flight path with the horizontal is 30°, angle of direction of thrust with the horizontal is 20° and mass of the vehicle is 300 kg. Assume the acceleration due to gravity to be 9.8 m/s2.
9. Determine the time period of revolution of a satellite in a circular orbit around a planet of radius 6374 m at a height of 600 m. Assume the acceleration due to gravity at sea level to be 9.8 m/s2.
10. How will propellant mass flow and thrust change with burn duration in a gravity-free, drag-free environment?
11. __________ is that part of a launch vehicle that carries the payload.
12. For a circular trajectory of a satellite around the earth, the centrifugal forces must balance the ______
13. Which of the following is acceleration perpendicular to the flight path?
14. What is the nature of the trajectory of rockets in gravity-free, drag-free environment?
15. What is the nature of the effect of the propellant mass fraction on the vehicle velocity?
16. Which of the following terms are not related to a strap-on stage of a rocket engine?
17. At which of the following altitudes does the infrared emissions from the mixing zone of the rocket exhaust higher?
18. Which of the following statements is true for the center of gravity (cog) and the center of pressure (cop) location along the axis of a fuel powered aircraft?
19. An example for an unpowered maneuvering is ___________
20. What kind of maneuvers are typically provided by the reaction control systems?
21. In the case of orbital transfer from one orbit to another, if the new orbit is higher, then the thrusts are applied in the opposite direction to the flight velocity vector.
22. Afterburning can lead to ozone layer depletion.
23. Determine the mass ratio (Initial mass/Burnout mass) for each stage for a 3-stage rocket, given the total velocity increment is 2000 m/s, mass ratio is constant for all stages and the exhaust velocity is constant for all stages with a value of 3000 m/s.
24. Why are the orbits of satellites outside of the earth’s atmosphere?
25. Rocket propulsion thrust vector passes through the ___________ of the vehicle.