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 15
... launch vehicle . Led by France , the Ariane program launched its first rocket on 24 December 1979 from its space center Kourou in French Guayana . The Ariane series of rockets is responsible for placing more than one - half of all ...
... launch vehicle . Led by France , the Ariane program launched its first rocket on 24 December 1979 from its space center Kourou in French Guayana . The Ariane series of rockets is responsible for placing more than one - half of all ...
Страница 218
... launch vehi- cle provider issues a payload interface document describing how and where the satellite can be attached to the launch vehicle . Some launch vehicle companies retain design ownership of the adapter assembly . The satellite ...
... launch vehi- cle provider issues a payload interface document describing how and where the satellite can be attached to the launch vehicle . Some launch vehicle companies retain design ownership of the adapter assembly . The satellite ...
Страница 220
... launch environment and on - orbit operational environment . The launch environment is characterized by □ High linear accelerations due to the vehicle acceleration ( 3 to 12 G's sustained ) . Shocks from stage separations and stage ...
... launch environment and on - orbit operational environment . The launch environment is characterized by □ High linear accelerations due to the vehicle acceleration ( 3 to 12 G's sustained ) . Shocks from stage separations and stage ...
Съдържание
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Авторско право | |
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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