Interactive Aerospace Engineering and DesignMcGraw-Hill, 2002 - 356 pages This text contains an integrated bound-in CD-ROM, and has a strong emphasis on design. Its active visual approach and inclusion of space-orientated engineering make it an interesting examination of the aerospace engineering field. |
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Page 218
... onboard thrusters for stability and control . A satellite bus is typically composed of the following subsystems that all interact to ensure the mission payload operates successfully [ 82 ] : Structures and mechanisms . Power ...
... onboard thrusters for stability and control . A satellite bus is typically composed of the following subsystems that all interact to ensure the mission payload operates successfully [ 82 ] : Structures and mechanisms . Power ...
Page 228
... onboard electronics , Earth IR , and albedo heat . Considering the thermal environment and input power , propose a valid satellite design . From Equation ( 8.3 ) , the power absorbed , or input , from the sun is Pabsorbed = α a ( z Ps ...
... onboard electronics , Earth IR , and albedo heat . Considering the thermal environment and input power , propose a valid satellite design . From Equation ( 8.3 ) , the power absorbed , or input , from the sun is Pabsorbed = α a ( z Ps ...
Page 231
... onboard . These are available for almost any mission ; however , the drift of the gyroscope associated with friction losses in the spinning mechanisms results in increasing measurement errors over time . Thus , the IMU needs to be ...
... onboard . These are available for almost any mission ; however , the drift of the gyroscope associated with friction losses in the spinning mechanisms results in increasing measurement errors over time . Thus , the IMU needs to be ...
Table des matières
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Droits d'auteur | |
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Expressions et termes fréquents
aerodynamic aerospace aircraft airfoil airplane altitude angle of attack antenna Apollo astronauts atmosphere balloon body calculated CD-ROM chapter coefficient components compressor crew member Decavitator defined density design process drag drawing ellipse energy Equation example Figure flight force fuel gravity human human spaceflight inlet International Space Station jet engine joint launch lift lines low Earth orbit LTA vehicle lunar magnetic field magnetosphere maneuver materials maximum microgravity mission module motion multiview NASA nozzle object onboard operational orbital mechanics oxygen parameters particles payload percent performance plane planetary pressure problem propeller propulsion radiation ratio rocket satellite semimajor axis simulation Skylab solar space environment Space Shuttle space station spacecraft spaceflight spacesuit design specific speed stability structural subsystem surface temperature thermal thrust turbine units Van Allen belts vector vehicle design velocity wing