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 166
... oxygen is more abun- dant than molecular oxygen or nitrogen . Atomic oxygen forms when solar ultra- violet radiation dissociates molecular oxygen . The nature of atomic oxygen is highly reactive due to its high chemical activity ...
... oxygen is more abun- dant than molecular oxygen or nitrogen . Atomic oxygen forms when solar ultra- violet radiation dissociates molecular oxygen . The nature of atomic oxygen is highly reactive due to its high chemical activity ...
Page 261
... oxygen pressure required for breathing and ventilation and protects the crew member against bright sunlight and temperature extremes . The LSS controls the internal oxygen pressure , makes up oxygen losses due to leakage and metab ...
... oxygen pressure required for breathing and ventilation and protects the crew member against bright sunlight and temperature extremes . The LSS controls the internal oxygen pressure , makes up oxygen losses due to leakage and metab ...
Page 281
... oxygen and minerals , propellants such as liquid oxygen , liquid hydrogen , and silane also have the potential for being man- ufactured on the Moon . On the Martian surface , like lunar regolith , the soil is rich in O2 and minerals ...
... oxygen and minerals , propellants such as liquid oxygen , liquid hydrogen , and silane also have the potential for being man- ufactured on the Moon . On the Martian surface , like lunar regolith , the soil is rich in O2 and minerals ...
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