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 179
... solar maximum , solar flares are often observed , and an active zone can be responsible for several consecutive solar flares . Sunspots tend to reside at high solar latitudes and remain at that latitude for the duration of their life ...
... solar maximum , solar flares are often observed , and an active zone can be responsible for several consecutive solar flares . Sunspots tend to reside at high solar latitudes and remain at that latitude for the duration of their life ...
Page 221
... solar panel under direct solar light ( i.e. , perpendicular to the sun's incident radi- ation ) . However , as satellites travel deeper into the solar system , the available solar energy flux decreases with the square of the distance ...
... solar panel under direct solar light ( i.e. , perpendicular to the sun's incident radi- ation ) . However , as satellites travel deeper into the solar system , the available solar energy flux decreases with the square of the distance ...
Page 351
... solar absorption coefficient , 167-69 solar arrays and satellites , 220 , 221–22 , 227 ( table ) tradeoffs , 242 solar constant , 167 solar cosmic rays ( SCRs ) , 177–79 solar flares , 178 , 179 , 181 solar proton events , 179 solar ...
... solar absorption coefficient , 167-69 solar arrays and satellites , 220 , 221–22 , 227 ( table ) tradeoffs , 242 solar constant , 167 solar cosmic rays ( SCRs ) , 177–79 solar flares , 178 , 179 , 181 solar proton events , 179 solar ...
Table des matières
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Droits d'auteur | |
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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