Interactive Aerospace Engineering and DesignMcGraw-Hill, 2002 - 356 Seiten 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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Seite 66
... exist , almost all are made up of the same basic components that either are fixed or move . Generally , the fixed components include the wings , a fuselage , a tail , engines , a vertical stabilizer , and a horizontal stabilizer . For ...
... exist , almost all are made up of the same basic components that either are fixed or move . Generally , the fixed components include the wings , a fuselage , a tail , engines , a vertical stabilizer , and a horizontal stabilizer . For ...
Seite 184
... exist to harden the satellite ( e.g. , through coatings , thermal conditioning , extra outside material layers ) . Regardless , a mete- oroid can be fatal to a spacecraft , and nothing can be done to prevent it except to spot the object ...
... exist to harden the satellite ( e.g. , through coatings , thermal conditioning , extra outside material layers ) . Regardless , a mete- oroid can be fatal to a spacecraft , and nothing can be done to prevent it except to spot the object ...
Seite 195
... exist from the ancient Babylonian civilization that possess cuneiform writing , illustrating the sexagesimal ( base - 60 ) system of notation that was used . This sys- tem of numeration remained in use through the time of Copernicus ...
... exist from the ancient Babylonian civilization that possess cuneiform writing , illustrating the sexagesimal ( base - 60 ) system of notation that was used . This sys- tem of numeration remained in use through the time of Copernicus ...
Inhalt
A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
Urheberrecht | |
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Häufige Begriffe und Wortgruppen
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
Verweise auf dieses Buch
Intelligent Components and Instruments for Control Applications 2003 (SICICA ... L. Almeida,Luis B. Almeida,S. Boverie Eingeschränkte Leseprobe - 2003 |