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. |
À l'intérieur du livre
Résultats 1-3 sur 69
Page 167
... body , such as a spacesuited astronaut during a spacewalk or a planet or a satellite , can transfer heat to or from another body solely by radiation , provided the body is in a state of thermal equilibrium . The term satellite is used ...
... body , such as a spacesuited astronaut during a spacewalk or a planet or a satellite , can transfer heat to or from another body solely by radiation , provided the body is in a state of thermal equilibrium . The term satellite is used ...
Page 168
... body . For a perfectly diffuse sphere , the effective area of absorption is the frontal area of the body fac- ing the Sun , expressed as # r2 , and the middle term in the equation is known as the solar irradiance or solar constant . For ...
... body . For a perfectly diffuse sphere , the effective area of absorption is the frontal area of the body fac- ing the Sun , expressed as # r2 , and the middle term in the equation is known as the solar irradiance or solar constant . For ...
Page 205
... body for a given position and time is the angular position subtended by a fictitious body traveling for the same amount of time on a circular orbit which possesses the same period as the original body's elliptical orbit constant rate ...
... body for a given position and time is the angular position subtended by a fictitious body traveling for the same amount of time on a circular orbit which possesses the same period as the original body's elliptical orbit constant rate ...
Table des matières
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Droits d'auteur | |
21 autres sections non affichées
Autres éditions - Tout afficher
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