Spacecraft Trajectories — MCQs August 20, 2025 by u930973931_answers 50 Score: 0 Attempted: 0/50 Subscribe 1. What is a spacecraft trajectory? (A) The spin rate of the spacecraft (B) The path a spacecraft follows under forces (C) The spacecraft’s communication pattern (D) The shape of a satellite 2. Which law primarily governs spacecraft trajectories? (A) Newton’s Second Law (B) Kepler’s Laws of Planetary Motion (C) Ohm’s Law (D) Hooke’s Law 3. A Hohmann transfer orbit is used for: (A) Interstellar travel (B) Efficient transfer between two circular orbits (C) Escape from the Solar System (D) Polar orbits 4. A gravity assist maneuver is also known as: (A) Rocket boost (B) Slingshot (C) Orbital decay (D) Aerobraking 5. Gravity assists allow spacecraft to: (A) Use less fuel (B) Gain speed (C) Change direction (D) All of the above 6. The escape velocity from Earth is approximately: (A) 5 km/s (B) 7.9 km/s (C) 11.2 km/s (D) 15 km/s 7. Which trajectory is used to escape the gravitational field of a planet? (A) Circular orbit (B) Elliptical orbit (C) Hyperbolic trajectory (D) Parabolic trajectory 8. A geostationary orbit requires a period of: (A) 12 hours (B) 24 hours (C) 48 hours (D) 6 hours 9. Which orbit keeps a satellite fixed above one point on Earth? (A) Polar orbit (B) Geostationary orbit (C) Elliptical orbit (D) Sun-synchronous orbit 10. A transfer orbit between Earth and Mars is typically: (A) Hohmann transfer (B) Hyperbolic escape (C) Circular parking orbit (D) Sun-synchronous orbit 11. Delta-v in spacecraft missions refers to: (A) Speed of light (B) Change in velocity (C) Fuel density (D) Orbital radius 12. Which orbit allows continuous coverage of polar regions? (A) Equatorial orbit (B) Sun-synchronous orbit (C) Geostationary orbit (D) Circular orbit 13. The Apollo missions to the Moon used a: (A) Direct hyperbolic transfer (B) Hohmann-like trajectory (C) Geostationary parking orbit (D) Elliptical low Earth orbit 14. Spacecraft trajectory corrections are done using: (A) Gyroscopes only (B) Star trackers only (C) Onboard propulsion (D) Solar sails only 15. A spacecraft on a parabolic trajectory has: (A) Less than escape energy (B) Exactly escape energy (C) More than escape energy (D) No orbital energy 16. Which type of orbit is typically used for weather satellites? (A) Geostationary (B) Sun-synchronous (C) Polar (D) All of the above 17. A Lagrange point is a region where: (A) Gravity is absent (B) Forces balance for stable spacecraft positions (C) Orbits decay quickly (D) Spacecraft accelerate rapidly 18. Which Lagrange point is used for the James Webb Space Telescope? (A) L1 (B) L2 (C) L3 (D) L4 19. A Molniya orbit is a type of: (A) Geostationary orbit (B) Highly elliptical orbit (C) Sun-synchronous orbit (D) Low Earth orbit 20. Aerobraking is used to: (A) Increase spacecraft velocity (B) Reduce velocity using a planet’s atmosphere (C) Generate power (D) Achieve escape velocity 21. The Interplanetary Transport Network uses: (A) Low-energy trajectories (B) Constant rocket thrust (C) Geostationary orbit transfers (D) Magnetic propulsion only 22. Orbital insertion involves: (A) Launching into orbit (B) Changing from one orbit to another (C) Entering a stable orbit around a planet (D) Exiting orbit 23. Which spacecraft used multiple gravity assists to reach Mercury? (A) Voyager 1 (B) Galileo (C) MESSENGER (D) New Horizons 24. Which trajectory allowed Voyager 2 to visit all four giant planets? (A) Gravity assist trajectory (B) Direct hyperbolic escape (C) Polar orbit (D) Hohmann transfer 25. The Oberth effect enhances: (A) Delta-v gained when thrusting near periapsis (B) Fuel efficiency at apogee (C) Orbital inclination (D) Gravitational constant 26. Which orbit is ideal for reconnaissance satellites? (A) Sun-synchronous orbit (B) Geostationary orbit (C) Highly elliptical orbit (D) Lagrange orbit 27. Escape trajectories are always: (A) Elliptical (B) Circular (C) Parabolic or hyperbolic (D) Geostationary 28. Which orbital maneuver is used to match orbital planes? (A) Inclination change (B) Hohmann transfer (C) Gravity assist (D) Oberth effect 29. Time of flight in a Hohmann transfer depends on: (A) Orbital radius (B) Inclination (C) Eccentricity (D) Mass of spacecraft 30. Which planet provides the strongest gravity assist in the Solar System? (A) Saturn (B) Neptune (C) Jupiter (D) Earth 31. The Tsiolkovsky rocket equation relates: (A) Velocity change, exhaust velocity, and mass ratio (B) Orbit period and radius (C) Mass and gravitational force (D) Power and thrust 32. A spacecraft in Low Earth Orbit (LEO) has an altitude of about: (A) 100–2,000 km (B) 5,000–10,000 km (C) 20,000–30,000 km (D) 36,000 km 33. GPS satellites are in which orbit? (A) LEO (B) MEO (C) GEO (D) Sun-synchronous 34. What is the approximate altitude of geostationary orbit? (A) 1,000 km (B) 5,000 km (C) 20,200 km (D) 35,786 km 35. A spacecraft approaching Mars must perform: (A) Aerobraking or orbital insertion burn (B) Direct descent (C) Solar sail maneuver (D) Gravity assist from Earth 36. What is a transfer window in interplanetary missions? (A) The best time for solar observation (B) The optimal launch period (C) A spacecraft hatch (D) A navigation system 37. Which spacecraft used a direct hyperbolic trajectory to Pluto? (A) Cassini (B) Voyager 1 (C) MESSENGER (D) New Horizons 38. Which maneuver is used for orbital altitude adjustments? (A) Plane change (B) Apoapsis/periapsis burn (C) Gravity assist (D) Aerobraking 39. A bi-elliptic transfer is more efficient than Hohmann when: (A) The ratio of final to initial orbit radii is large (B) The spacecraft is in LEO (C) Launching to the Moon (D) Inclination is small 40. Which mission used Earth flybys to gain energy toward Saturn? (A) Voyager 1 (B) Galileo (C) Cassini (D) New Horizons 41. Interplanetary trajectories are computed using: (A) Two-body approximation (B) N-body simulations (C) Patched conics method (D) All of the above 42. The delta-v budget for a mission refers to: (A) Launch mass (B) Available velocity change capability (C) Number of engines (D) Orbital eccentricity 43. A spacecraft in a parking orbit is: (A) Orbiting Earth temporarily before transfer (B) Waiting at Lagrange points (C) On escape trajectory (D) In hyperbolic motion 44. Which orbit is best for communications with polar regions? (A) Sun-synchronous orbit (B) Geostationary orbit (C) Molniya orbit (D) Equatorial orbit 45. Which factor strongly affects re-entry trajectory? (A) Speed and angle of entry (B) Magnetic field strength (C) Solar wind (D) Communication frequency 46. The trajectory correction maneuver (TCM) is applied: (A) During launch (B) During cruise phase (C) During re-entry (D) After landing 47. Which orbit is most suitable for Earth observation satellites? (A) Sun-synchronous orbit (B) Geostationary orbit (C) High Earth orbit (D) Lagrange orbit 48. A free-return trajectory was used in: (A) Voyager (B) Apollo 11 (C) Apollo 13 (D) Cassini 49. Which is a key challenge in trajectory design? (A) Fuel constraints (B) Gravity assists timing (C) Orbital mechanics (D) All of the above 50. Spacecraft trajectory planning combines: (A) Physics, engineering, and computational methods (B) Astronomy only (C) Chemistry only (D) Biology and geology