Interactive Aerospace Engineering and DesignMcGraw-Hill, 2002 - 356 страници 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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Страница 216
... satellite ( uplink ) , which then transmits the information down to another switch elsewhere in the world ( downlink ) , and then data are sent via terrestrial lines to the ... Satellite Systems Engineering An Operational Satellite System.
... satellite ( uplink ) , which then transmits the information down to another switch elsewhere in the world ( downlink ) , and then data are sent via terrestrial lines to the ... Satellite Systems Engineering An Operational Satellite System.
Страница 218
... satellite can be attached to the launch vehicle . Some launch vehicle companies retain design ownership of the adapter assembly . The satellite designer plans according to three ... Satellite Systems Engineering Satellite Bus Subsystems.
... satellite can be attached to the launch vehicle . Some launch vehicle companies retain design ownership of the adapter assembly . The satellite designer plans according to three ... Satellite Systems Engineering Satellite Bus Subsystems.
Страница 232
... Satellite orbit change . Angular - momentum management . □ Satellite end - of - life ( EOL ) disposal . Initial spin - up is performed on spin - stabilized satellites , whose large angu- lar momentum is used to provide stability . The ...
... Satellite orbit change . Angular - momentum management . □ Satellite end - of - life ( EOL ) disposal . Initial spin - up is performed on spin - stabilized satellites , whose large angu- lar momentum is used to provide stability . The ...
Съдържание
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Авторско право | |
21 други раздела не са показани
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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