Interactive Aerospace Engineering and DesignThis 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. |
From inside the book
Results 1-3 of 9
Page 204
... semi- major axis and its eccentricity . The semimajor axis a of an ellipse can be described as one - half the length of the longitudinal axis of the ellipse . The eccen- tricity e defines the shape of the orbit ; it is quantified as the ...
... semi- major axis and its eccentricity . The semimajor axis a of an ellipse can be described as one - half the length of the longitudinal axis of the ellipse . The eccen- tricity e defines the shape of the orbit ; it is quantified as the ...
Page 211
... Semimajor axis : one - half the length of the major axis b - Semiminor axis : one - half the length of the minor axis h - Massless angular momentum : magnitude of radius crossed with velocity μ - Gravitational constant multiplied by the ...
... Semimajor axis : one - half the length of the major axis b - Semiminor axis : one - half the length of the minor axis h - Massless angular momentum : magnitude of radius crossed with velocity μ - Gravitational constant multiplied by the ...
Page 212
... semimajor axis ? Is the mass of the planet important ? Qualitative explanations are fine . 9.4 For an elliptical orbit , the point of closest approach to the central body is called the periapsis , and the point of greatest distance from ...
... semimajor axis ? Is the mass of the planet important ? Qualitative explanations are fine . 9.4 For an elliptical orbit , the point of closest approach to the central body is called the periapsis , and the point of greatest distance from ...
Contents
A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
Copyright | |
15 other sections not shown
Other editions - View all
Common terms and phrases
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