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. |
Между кориците на книгата
Резултати 1 - 3 от 62.
Страница 201
... energy of the system is the same thing as the force function and is denoted by U. The concepts of potential energy and kinetic energy are familiar from physics , and the link to orbital mechanics will become evident . If we define the ...
... energy of the system is the same thing as the force function and is denoted by U. The concepts of potential energy and kinetic energy are familiar from physics , and the link to orbital mechanics will become evident . If we define the ...
Страница 218
... energy source of the satellite . It is usually com- posed of two energy systems , namely , a short - term energy system and a long- term energy system . The short - term energy system is used for prelaunch and ini- tial orbit ...
... energy source of the satellite . It is usually com- posed of two energy systems , namely , a short - term energy system and a long- term energy system . The short - term energy system is used for prelaunch and ini- tial orbit ...
Страница 221
... energy ; store energy ; and regulate , distribute , and control power flow . Early spacecraft carried battery packs that would provide low voltage for a matter of hours or days , after which the satellite would be inoperable . It was ...
... energy ; store energy ; and regulate , distribute , and control power flow . Early spacecraft carried battery packs that would provide low voltage for a matter of hours or days , after which the satellite would be inoperable . It was ...
Съдържание
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Авторско право | |
21 други раздела не са показани
Други издания - Преглед на всички
Често срещани думи и фрази
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