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 121
... thermal efficiency is governed by thermodynamics . We can show that the thermal efficiency is less than the Carnot ( ideal ) efficiency . η ≤nc = 1 - To Tsource [ 6.7 ] For the atmosphere the mean temperature To ranges between 200 and ...
... thermal efficiency is governed by thermodynamics . We can show that the thermal efficiency is less than the Carnot ( ideal ) efficiency . η ≤nc = 1 - To Tsource [ 6.7 ] For the atmosphere the mean temperature To ranges between 200 and ...
Page 228
... thermal designer for a satellite team . There is an aluminum spherical satellite floating in orbit , which we call MetalSat . For this example , we assume no major thermal inputs from onboard electronics , Earth IR , and albedo heat ...
... thermal designer for a satellite team . There is an aluminum spherical satellite floating in orbit , which we call MetalSat . For this example , we assume no major thermal inputs from onboard electronics , Earth IR , and albedo heat ...
Page 353
... thermal conduction , 221 thermal control for cosmonauts , 267-68 and satellites , 226-27 on satellites , 219 , 228-29 thermal efficiency , 120-21 thermal meteoroid garment , 264 thermal stress , 220 thermosphere , 166 thinking , like ...
... thermal conduction , 221 thermal control for cosmonauts , 267-68 and satellites , 226-27 on satellites , 219 , 228-29 thermal efficiency , 120-21 thermal meteoroid garment , 264 thermal stress , 220 thermosphere , 166 thinking , like ...
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