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 38
... payload ( i.e. , pilot , passengers , and basket for hot - air balloons ) . These forces are expressed by the following : W = gas Pint & D πD2 4 W payload = Mpayload8 [ 3.6 ] [ 3.7 ] where weight is W , mass is m , Pint is the density ...
... payload ( i.e. , pilot , passengers , and basket for hot - air balloons ) . These forces are expressed by the following : W = gas Pint & D πD2 4 W payload = Mpayload8 [ 3.6 ] [ 3.7 ] where weight is W , mass is m , Pint is the density ...
Page 216
... payload ( see Section 10.3 , " Elements of a Satellite , " for pay- load details ) . The uplink provides ground controllers with the capability to send command information to the satellite to perform certain functions such as orbit ...
... payload ( see Section 10.3 , " Elements of a Satellite , " for pay- load details ) . The uplink provides ground controllers with the capability to send command information to the satellite to perform certain functions such as orbit ...
Page 217
... payload , the bus , and the launch vehicle adapter assembly . The payload is defined as the equipment that performs the satellite mission function . For example , a telecommunication satel- lite's payload would be defined as the ...
... payload , the bus , and the launch vehicle adapter assembly . The payload is defined as the equipment that performs the satellite mission function . For example , a telecommunication satel- lite's payload would be defined as the ...
Table des matières
A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
Droits d'auteur | |
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Expressions et termes fréquents
aerodynamic aircraft airfoil airplane altitude angle of attack antenna Apollo astronauts atmosphere axis balloon body Boeing burner calculate camber CD-ROM chapter coefficient coefficient of lift components compressor crew member debris Decavitator drag drawing efficiency elliptical energy Equation equilibrium example Figure flight force freestream fuel gravity human human spaceflight inlet International Space Station jet engine joint launch lift load factor low Earth orbit LTA vehicle lunar maneuver mass flow materials maximum microgravity mission motion NASA nozzle object operational orbital mechanics oxygen particles payload performance plane planetary pressure problem produced propeller propulsion radiation ratio rocket satellite semimajor axis simulation Skylab solar space environment Space Shuttle space station spacecraft spaceflight specific speed stability static structural surface temperature thermal thrust truss turbine turbofan turbojet United vector velocity wing