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 171
... Earth ( like the International Space Station ) are nowhere near far enough away to avoid Earth's gravitational field — they are only about 300 km above the surface of Earth ( less than one - tenth of one Earth radius ) ... Low Earth Orbit.
... Earth ( like the International Space Station ) are nowhere near far enough away to avoid Earth's gravitational field — they are only about 300 km above the surface of Earth ( less than one - tenth of one Earth radius ) ... Low Earth Orbit.
Page 173
... Low Earth orbit , or LEO , is the term used to define orbits used for human spaceflight and some satellites , which are rather close to Earth ( ~ 300 to 1,000s km altitude ) . By flying in an orbit close to Earth , astronauts avoid ...
... Low Earth orbit , or LEO , is the term used to define orbits used for human spaceflight and some satellites , which are rather close to Earth ( ~ 300 to 1,000s km altitude ) . By flying in an orbit close to Earth , astronauts avoid ...
Page 187
... Orbital debris is becoming a major concern for those planning spacecraft mis- sions in Earth orbit , either in low Earth orbit ( LEO ) or in geosynchronous Earth orbit ( GEO ) . It is a growing concern as constellations of dozens and ...
... Orbital debris is becoming a major concern for those planning spacecraft mis- sions in Earth orbit , either in low Earth orbit ( LEO ) or in geosynchronous Earth orbit ( GEO ) . It is a growing concern as constellations of dozens and ...
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