Introduction to Aerospace Engineering Mid - II, November - 2014
1.If the forces and moments on the body caused by a disturbance tend initially to return the body toward its equilibrium position is called as
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statically stable
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dynamically stable
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both a & b
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resulting forces
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Answer: A
2.An airplane is in pitch equilibrium when the _______________
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Mcg = CM, cg = 0
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Mac = CM, ac = 1
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Mac = CM, ac = 0
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Mac = CM, cg = 0
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Answer: A
3.The data storage center is the main storehouse of
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Uplinked information
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downlinked information
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both a & b
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None
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Answer: B
4._______uses angular momentum of the rotating satellite to maintain stability and control
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spin-stabilized satellites
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3-axis stabilized satellites
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De-stabilized satellites
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all
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Answer: A
5.The _____________________ is responsible for maintaining the components of the satellite within operational temperature limits.
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Power subsystem
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thermal control subsystem
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attitude determination and control subsystem
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Propulsion and station-keeping subsystem
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Answer: B
6.Scientific missions are initiated with the intent to____________________
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Discover
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Protect, monitor, and learn
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help society
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telecommunications
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Answer: A
7.Total emitted or radiated power is given by
Answer: D
8.One of the challenging problems to solve in the early stages of a design is how to represent __objects on a __ surface.
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3D, 2D
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2D, 3D
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big, small
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high, low
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Answer: A
9.A _________is a method to represent a 3D object by extending all its points with straight lines to a plane of projection.
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Design
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projection
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Both a & b
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Representation
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Answer: B
10.______________is an extension of CAD usually following from solid modeling, in which the tool paths for fabrication are defined within the computer model.
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Computer-aided machining
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Mechanism Design
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Finite Element Meshing
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Systems Analysis
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Answer: A
11.Satellite missions are categorized into ______________________________
Answer: Scientific, Military and national security, Civil & Commercial.
12.The __________&__________is responsible for processing the raw downlinked data into some form of interpretable information.
Answer: data analysis and distribution center
13.The satellite designer plans according to three budgets: ________________________
Answer: The mass budget, the power budget, and the cost budget
14.The ____________________________functions to keep the satellite in its intended orbit.
Answer: Propulsion and station-keeping subsystem
15.IMU: ___________________
Answer: Inertial measurement unit.
16.Life support functions fall into two categories:_________________________.
Answer: Non-regenerative and regenerative
17.The design is beginning to formulate on a systems level, and the analysis will help to verify the ___________________statement.
Answer: original problem
18.The __________________design provides an opportunity for the concepts and approaches of aerospace engineering in the context of the design.
Answer: lighter-than-air vehicle
19.WRM : ____________________________________
Answer: Water recovery and management
20.___________________________________are basic functions that are part of most scenarios for future human missions.
Answer: Atmosphere production, revitalization, and water recovery