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 249
... lunar orbiting missions , a lunar swingby , and six Moon landing missions . The Apollo program was designed to land humans on the Moon and bring them Kennedy.mpg safely back to Earth . Six of the missions ( Apollos 11 , 12 , 14 , 15 ...
... lunar orbiting missions , a lunar swingby , and six Moon landing missions . The Apollo program was designed to land humans on the Moon and bring them Kennedy.mpg safely back to Earth . Six of the missions ( Apollos 11 , 12 , 14 , 15 ...
Page 272
... lunar environment , but his recom- mendations for future planetary spacesuits should be heeded . Jones and Schmitt [ 125 ] suggest that improvements in mobility and suit flexibility will have a sig- nificant impact on astronaut ...
... lunar environment , but his recom- mendations for future planetary spacesuits should be heeded . Jones and Schmitt [ 125 ] suggest that improvements in mobility and suit flexibility will have a sig- nificant impact on astronaut ...
Page 276
... lunar gravity showing a significant reduction in peak force ( fmax ) for each stride during Martian and lunar locomotion as compared to 1 G locomotion . The time of foot ground contact is denoted by te , time of flight ( or aerial time ...
... lunar gravity showing a significant reduction in peak force ( fmax ) for each stride during Martian and lunar locomotion as compared to 1 G locomotion . The time of foot ground contact is denoted by te , time of flight ( or aerial time ...
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