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. |
À l'intérieur du livre
Résultats 1-3 sur 35
Page 171
... less than that on Earth , or 1 × 10-6 Gs - nearly , but not quite , weightless . Microgravity Calculation Let us calculate how far away we would need to be from Earth to achieve this micro- gravity , or near - weightless , condition ...
... less than that on Earth , or 1 × 10-6 Gs - nearly , but not quite , weightless . Microgravity Calculation Let us calculate how far away we would need to be from Earth to achieve this micro- gravity , or near - weightless , condition ...
Page 190
... less massive , we expect to see a greater loss of atmospheric gas until , finally , we see a loss of atmosphere all together . Martian Environment The Martian atmosphere has a typical surface pressure of about 0.01 of Earth's atmosphere ...
... less massive , we expect to see a greater loss of atmospheric gas until , finally , we see a loss of atmosphere all together . Martian Environment The Martian atmosphere has a typical surface pressure of about 0.01 of Earth's atmosphere ...
Page 255
... less than previously thought and will not significantly disturb the ISS microgravity environment [ 112 ] . These are very low forces when compared to typical Earth forces . Actually , they are an order of magnitude less . For example ...
... less than previously thought and will not significantly disturb the ISS microgravity environment [ 112 ] . These are very low forces when compared to typical Earth forces . Actually , they are an order of magnitude less . For example ...
Table des matières
A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
Droits d'auteur | |
15 autres sections non affichées
Autres éditions - Tout afficher
Expressions et termes fréquents
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