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Spacecraft design - Test
Contributed by: Leigh
  • 1. Spacecraft design involves the intricate planning and engineering of vehicles intended for travel or operation in outer space. It encompasses a wide range of disciplines, including aerospace engineering, systems engineering, materials science, and computer science. Design considerations include structural integrity, propulsion systems, thermal protection, life support systems, and communication systems. Spacecraft must be carefully designed to withstand the harsh conditions of space, including extreme temperatures, radiation, and microgravity, while also ensuring efficiency, reliability, and safety for crew members or payloads. The design process is highly iterative, involving iterative modeling, simulation, and testing to optimize performance and minimize risks. Successful spacecraft design is crucial for the success of space exploration missions, satellite deployments, and scientific research in space.

    What is the purpose of a heat shield on a spacecraft?
A) To create artificial gravity inside the spacecraft
B) To harvest solar energy
C) To communicate with the ground control
D) To protect the spacecraft from high temperatures during reentry
  • 2. What system is responsible for maintaining a spacecraft's orientation in space?
A) Attitude control system
B) Life support system
C) Navigation system
D) Propulsion system
  • 3. What is the purpose of a star tracker on a spacecraft?
A) To determine the spacecraft's orientation by locating stars
B) To collect samples from asteroids
C) To generate electricity from sunlight
D) To communicate with other spacecraft
  • 4. Which type of propulsion system is commonly used for maneuvering spacecraft during missions?
A) Solar sail propulsion
B) Nuclear propulsion
C) Ion propulsion
D) Chemical propulsion
  • 5. What is the purpose of a lander on a planetary exploration spacecraft?
A) To communicate with satellites
B) To collect solar energy
C) To safely descend and land on the planetary surface
D) To conduct experiments in orbit
  • 6. Which design concept involves placing multiple smaller satellites into orbit together to perform a common mission?
A) Single point design
B) Megastructure
C) Constellation
D) Orbital platform
  • 7. What does a spacecraft's thermal control system help regulate?
A) Fuel consumption
B) Temperature
C) Speed
D) Orbit
  • 8. What do spacecraft designers consider to protect sensitive components from radiation in space?
A) Shielding materials
B) Communication antennas
C) Solar panels
D) Thermal blankets
  • 9. Which type of propulsion system is used to adjust the orbit of satellites over a long period of time?
A) Chemical propulsion
B) Solar sail propulsion
C) Fission propulsion
D) Electric propulsion
  • 10. What helps protect a spacecraft from micrometeoroids and space debris?
A) Lithium-ion batteries
B) Solar panels
C) Whipple shields
D) Antennas
  • 11. What does RCS stand for in the context of spacecraft design?
A) Reentry Capsule System
B) Reaction Control System
C) Radio Communication System
D) Remote Control System
  • 12. What is the purpose of a deployable boom on a spacecraft?
A) To store additional propellant
B) To extend sensors away from the spacecraft's body
C) To generate electricity
D) To communicate with Earth
  • 13. What is a critical aspect of a spacecraft's power system to ensure continuous operation?
A) Efficiency
B) Redundancy
C) Speed
D) Weight
  • 14. Which component of a spacecraft is responsible for generating electricity from sunlight?
A) Batteries
B) Thrusters
C) Reactors
D) Solar panels
  • 15. What is the primary function of a spacecraft's avionics system?
A) To control and monitor the spacecraft's functions
B) To regulate temperature
C) To navigate in space
D) To provide propulsion
  • 16. What is the primary purpose of a payload fairing on a launch vehicle?
A) To communicate with the spacecraft
B) To protect the spacecraft during launch and ascent through Earth's atmosphere
C) To store extra fuel
D) To provide power to the spacecraft
  • 17. What is the primary function of a spacecraft's attitude control system?
A) To generate electricity
B) To orient the spacecraft in space
C) To store scientific data
D) To provide life support for the crew
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