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 36
... considered ; rather , rocket propulsion provides the thrust or lift of the spacecraft , which is not considered further . The two primary sources of drag discussed in this chapter include profile drag and induced drag . 3.2 GENERATING ...
... considered ; rather , rocket propulsion provides the thrust or lift of the spacecraft , which is not considered further . The two primary sources of drag discussed in this chapter include profile drag and induced drag . 3.2 GENERATING ...
Страница 166
... considered . Atmospheric drag makes orbiting Earth below 200 km not viable ; that is , a satellite at 200 km cannot remain there for more than several days ( the orbit duration depends on the ratio of surface area to mass of the ...
... considered . Atmospheric drag makes orbiting Earth below 200 km not viable ; that is , a satellite at 200 km cannot remain there for more than several days ( the orbit duration depends on the ratio of surface area to mass of the ...
Страница 284
... considered the most important factors contributing to the nature of the design to be those associated with the final outcome or end product . Under this system , projects were assigned and then taken to studios to be worked on with lit ...
... considered the most important factors contributing to the nature of the design to be those associated with the final outcome or end product . Under this system , projects were assigned and then taken to studios to be worked on with lit ...
Съдържание
A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
Авторско право | |
15 други раздела не са показани
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Често срещани думи и фрази
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