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 237
... module . The satellite bus design was taken from an existing multi- mission modular spacecraft ( MMS ) , and it consists of four primary modules and two submodules . The primary modules include the power , altitude control , com- mand ...
... module . The satellite bus design was taken from an existing multi- mission modular spacecraft ( MMS ) , and it consists of four primary modules and two submodules . The primary modules include the power , altitude control , com- mand ...
Page 249
... Module , and 9 , which tested both the Command Module and Lunar Module , were Earth orbiting missions . Apol- los 8 and 10 tested critical components while orbiting the Moon and returned photography of the lunar surface . Apollo 13 did ...
... Module , and 9 , which tested both the Command Module and Lunar Module , were Earth orbiting missions . Apol- los 8 and 10 tested critical components while orbiting the Moon and returned photography of the lunar surface . Apollo 13 did ...
Page 293
... MODULE - RUSSIA Selvering a meal Camera X - ray and telescopes OBSERVATION MODULE US raviolet Astro- orientation equipament Optical Exploded docking port CONNECTING MODULE The aim of space agriculture is to deliver nutrients and monitor ...
... MODULE - RUSSIA Selvering a meal Camera X - ray and telescopes OBSERVATION MODULE US raviolet Astro- orientation equipament Optical Exploded docking port CONNECTING MODULE The aim of space agriculture is to deliver nutrients and monitor ...
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