Our team has conducted extensive research to compile a set of Flight Vehicle Engineering MCQs. We encourage you to test your Flight Vehicle Engineering knowledge by answering these multiple-choice questions provided below.
Simply scroll down to begin!
A. Air to Ground Link
B. Average Ground Level
C. Adjusted Gross Landing
D. Above Ground Level
A. Mean sea level
B. Average terrain
C. Above ground level
D. Ground level
A. Grams per cubic meter OR grams per kilogram
B. Feet
C. Miles
D. Inches
A. Zero
B. -3
C. 3
D. 6
A. Metre per second squared (m s−2)
B. Seconds squared
C. Miles per hour
D. Feet per minute
A. Momentum
B. Force
C. Acceleration
D. Speed
A. Loss of signal
B. Acquisition of signal
C. Deserted satellite
D. End of pass
A. True
B. False
A. Automatic direction finder
B. Advanced data format
C. All-digital forum
D. Asynchronous data flow
A. A regular 2D camera
B. A computer vision system not designed for the International Space Station
C. A computer vision system designed for the International Space Station
D. A system that uses regular 2D cameras to calculate the 3D position of an object
A. Aerodynamic forces
B. Fluid motion
C. Aeolian tones
D. Noise generation
A. Slows the spacecraft
B. Reduces the high point of an elliptical orbit
C. Increases the high point of an elliptical orbit
D. Decreases the low point of an elliptical orbit
A. An unpowered aerostat that remains aloft or floats due to its buoyancy
B. An unpowered aerostat that does not float
C. A balloon that is tethered to a fixed point
D. A powered aerostat
A. A cone-shaped balloon
B. A toroidal burble fence
C. A balloon-like braking device
D. A parachute-like braking device
A. Microwave or laser beam
B. Gamma ray beam
C. X-ray beam
D. Ultraviolet beam
A. 180 degrees
B. 90 degrees
C. 360 degrees
D. 0 degrees
A. A decrease in pressure
B. A decrease in the fluid's potential energy
C. An increase in the fluid's density
D. A decrease in the fluid's density
A. 2
B. 1
C. 3
D. 4
A. The exhaust produced by gas turbine engines
B. A type of fuel used in gas turbine engines
C. A measure of the efficiency of gas turbine engines
D. Compressed air that is taken from the compressor stage of gas turbine engines
A. A rocket used to launch a multistage launch vehicle
B. A rocket used to augment the space vehicle's takeoff thrust and payload capability
C. A rocket used to provide thrust for a space vehicle
D. A rocket used for guidance for a space vehicle
A. The layer of fluid in the immediate vicinity of a bounding surface where the effects of gravity are significant
B. The layer of fluid in the immediate vicinity of a bounding surface where the effects of temperature are significant
C. The layer of fluid in the immediate vicinity of a bounding surface where the effects of buoyancy are significant
D. The layer of fluid in the immediate vicinity of a bounding surface where the effects of viscosity are significant
A. Upward force exerted by a fluid that opposes the weight of an immersed object
B. A fluid's resistance to change in shape
C. The pressure at the bottom of a column of fluid
D. The property of a fluid that causes it to rise to the highest point in a container
A. Loss in volume
B. Upthrust
C. Net force downwards
D. Net force upwards
A. Equal to
B. Greater
C. Less than
D. Twice as great
A. From the jet engines at the turbine stage
B. From the landing gear at the axle stage
C. From the propellers at the turbine stage
D. From the gas turbine engines at the compressor stage
A. Jet fuel
B. On board generators
C. Bled off from the gas turbine engines at the compressor stage
D. Carried in high-pressure, often cryogenic tanks
A. A method of data transmission
B. A method for tying wiring harnesses and cable looms
C. A type of cable
D. A device used to cut cable
A. Cable ties
B. Hook and loop Cable ties
C. Cable lacing
D. Cable management
A. The curved line formed by the intersection of a cone and a plane
B. The force required to move an object up a slope
C. The distance between the bottom of an object and the ground
D. The asymmetric curves on the top and bottom, or front and back, of an aerofoil
A. Up and down
B. Top and bottom
C. Left and right
D. Front and back
A. An aircraft with a canard configuration
B. A small forewing or foreplane placed forward of the main wing of a fixed-wing aircraft
C. The main wing of a fixed-wing aircraft
D. The foreplane of a fixed-wing aircraft
A. Center of Pressure
B. Center of Momentum
C. Center of Mass
D. Center of Gravity
A. Torque
B. Gradient
C. Axis
D. Gravity
A. To account for the torque caused by the variation in gravitational field
B. To calculate the satellite's altitude
C. To determine the satellite's orbital period
D. To calculate the satellite's velocity
A. The point where the weighted relative position of the distributed mass sums to zero.
B. The distribution of mass is balanced around the center of mass.
C. The average of the weighted position coordinates of the distributed mass defines its coordinates.
A. Leading edge and nose
B. Trailing edge and wingtip
C. Trailing edge and root chord
D. Leading edge and trailing edge
A. When its external equipment is turned off.
B. When its external equipment is retracted to minimize drag and thus maximize airspeed for a given power setting.
C. When its external equipment is set to minimum.
D. When its external equipment is removed.
A. The area from which a copilot controls the aircraft.
B. The area from which a navigator controls the aircraft.
C. The area from which a pilot controls the aircraft.
D. The area from which a flight attendant controls the aircraft.
A. Cockpit
B. Crew rest area
C. Emergency exit
D. Cargo hold
A. Laser beam
B. Refractor telescope
C. Perfectly collimated light beam
D. Diffraction grating
A. An icy, small Solar System body that, when passing close to the Sun, warms and begins to release gases.
B. A gas giant
C. A luminous object in the sky
D. A star with a tail
A. Reduce its size in one or more directions
B. Displace layers of the material parallel to each other
C. Increase its size in one or more directions
D. Have no net sum or torque directed
A. True
B. False
A. True
B. False
A. Single-speed drive
B. Variable speed drive
C. Multi-speed drive
D. Constant speed drive
A. True
B. False
A. The discipline of controls overlaps and is usually taught along with electrical engineering at many institutions around the world.
B. A branch of engineering that deals with the design of control systems.
C. A branch of engineering that applies automatic control theory to design systems with desired behaviors in control environments.
D. A branch of engineering that deals with the application of automatic control theory to the design of systems.
A. It is a reference to a different source
B. It is an estimated figure
C. It is an incorrect figure
D. It is a range
A. Mach 2
B. The lower critical Mach number
C. Mach 1
D. The upper critical Mach number
A. Almost equal
B. Equal
C. Greater than
D. Less than