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 13
... rocket program with Wernher von Braun serving as the top civilian specialist . In 1936 , the German military provided funding for a rocket research center at the island of Usedom near Pennemünde . It grew to become a rocket development ...
... rocket program with Wernher von Braun serving as the top civilian specialist . In 1936 , the German military provided funding for a rocket research center at the island of Usedom near Pennemünde . It grew to become a rocket development ...
Page 141
... rocket unbalances the forces , and the rocket travels upward . Later , when the rocket runs out of fuel , it slows down , stops at the highest point of its flight , then falls back to Earth . Applying Newton's second law to rocket ...
... rocket unbalances the forces , and the rocket travels upward . Later , when the rocket runs out of fuel , it slows down , stops at the highest point of its flight , then falls back to Earth . Applying Newton's second law to rocket ...
Page 142
... rocket engines use liquid propellants . Liquid propellants , which are often gases that have been chilled until they condense into liquids , are kept in separate containers : one for the fuel and the other for the oxidizer . Then , when ...
... rocket engines use liquid propellants . Liquid propellants , which are often gases that have been chilled until they condense into liquids , are kept in separate containers : one for the fuel and the other for the oxidizer . Then , when ...
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