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Satellite Communication Quiz 2

Total questions: 30

Worksheet time: 15mins

Name
Class
Date
1.

What is the primary function of the Attitude and Orbit Control System (AOCS)?

a)

To provide power to the satellite

b)

To control the orbit and stabilization of the satellite

c)

To transmit data to Earth

d)

To monitor the satellite's health

2.

Which subsystem is responsible for monitoring and controlling satellite operations?

a)

Power Supply System

b)

Attitude Control System

c)

Telemetry, Tracking, Command and Monitoring System (TTC&M)

d)

Communications Subsystem

3.

What type of thruster uses bipropellants like Mono-methyl Hydrazine?

a)

Ion thrusters

b)

Solar thrusters

c)

Arcjets

d)

Traditional bipropellant thruster

4.

What is the main purpose of the telemetry system?

a)

To track the satellite's position

b)

To convey measurement information from the satellite

c)

To control the satellite's orbit

d)

To provide power to the satellite

5.

Which type of sensor is used for attitude control in satellites?

a)

Pressure sensor

b)

Earth sensor

c)

Temperature sensor

d)

Magnetic sensor

6.

What is the maximum efficiency of solar cells used in satellites?

a)

10% to 12%

b)

12% to 15%

c)

15% to 20%

d)

20% to 25%

7.

What is the role of the propulsion system in the AOCS?

a)

To provide electrical power

b)

To control the satellite's orbit

c)

To maintain stabilization and position

d)

To transmit data

8.

Which type of antenna is known for high gain and narrow beam?

a)

Wire Antenna

b)

Reflector Antenna

c)

Phased Array Antenna

d)

Horn Antenna

9.

What is the primary advantage of three-axis body stabilization?

a)

Lower mass

b)

No spin required for payloads

c)

Simplicity

d)

Easier to control

10.

What does the acronym TTC&M stand for?

a)

Transmission, Tracking, Control and Management

b)

Telemetry, Transfer, Command and Monitoring

c)

Telemetry, Tracking, Command and Monitoring

d)

Tracking, Telemetry, Control and Management

11.

Which gravitational force affects satellites in geostationary orbit the most?

a)

Moon's gravitational force

b)

Earth's gravitational force

c)

Sun's gravitational force

d)

Mars' gravitational force

12.

What is the main disadvantage of three-axis stabilization?

a)

Increased complexity

b)

Lower accuracy

c)

Higher power consumption

d)

Increased weight

13.

What is the function of a transponder in satellite communication?

a)

To monitor satellite health

b)

To control the satellite's orbit

c)

To amplify and translate signals

d)

To generate power

14.

What type of transponder is suitable only for digital signals?

a)

Regenerative Transponder

b)

Bent Pipe Transponder

c)

Analog Transponder

d)

Passive Transponder

15.

What is the purpose of the solar array in a satellite?

a)

To control the satellite's position

b)

To monitor the satellite's health

c)

To generate electrical power

d)

To provide communication

16.

What is the typical power generation capacity of satellite solar cells?

a)

2 to 3 KW

b)

0.5 to 1 KW

c)

3 to 4 KW

d)

1 to 2 KW

17.

What is the main function of the power supply control circuit?

a)

To monitor satellite health

b)

To track the satellite's position

c)

To control electrical power distribution

d)

To provide propulsion

18.

What is the main challenge of operating in outer space?

a)

Low gravity

b)

High temperatures

c)

High radiation

d)

Harsh environment

19.

What is the purpose of the Earth sensor in a satellite?

a)

To control the satellite's orbit

b)

To detect solar radiation

c)

To sense infrared rays from the horizon

d)

To monitor temperature

20.

What is the typical inclination of the moon's orbit to the equatorial plane?

a)

5 degrees

b)

15 degrees

c)

3 degrees

d)

10 degrees

21.

What is the main purpose of the thermal control system in a satellite?

a)

To monitor satellite health

b)

To provide power

c)

To maintain temperature within operational limits

d)

To control the satellite's orbit

22.

What is the main advantage of using solar cells in satellites?

a)

High efficiency

b)

Lightweight

c)

Low cost

d)

Renewable energy source

23.

What is the main function of the command system in TTC&M?

a)

To convey measurement information

b)

To track the satellite's position

c)

To provide power

d)

To establish and maintain control

24.

What is the purpose of the quality control process in satellite manufacturing?

a)

To simplify design

b)

To increase weight

c)

To ensure reliability of components

d)

To reduce costs

25.

What is the primary function of the communications subsystem in a satellite?

a)

To monitor satellite health

b)

To provide power to the satellite

c)

To control the satellite's orbit

d)

To transmit data to Earth

26.

What type of power source is commonly used in satellites for energy storage?

a)

Nickel-Cadmium batteries

b)

Lead-acid batteries

c)

Lithium-ion batteries

d)

Alkaline batteries

27.

What is the main purpose of the satellite's thermal control system?

a)

To generate power

b)

To maintain optimal temperature for components

c)

To control the satellite's position

d)

To monitor the satellite's health

28.

What is the primary advantage of using a phased array antenna in satellite communication?

a)

Easy to manufacture

b)

Compact size

c)

High directivity

d)

Low cost

29.

What is the typical lifespan of a geostationary satellite?

a)

5 to 10 years

b)

20 to 25 years

c)

10 to 15 years

d)

15 to 20 years

30.

What is the main purpose of the satellite's attitude determination system?

a)

To control the satellite's power

b)

To determine the satellite's orientation

c)

To manage thermal conditions

d)

To facilitate communication