Question #36698

objects in the elliptical orbit the position farther from the gravity source is called the apogee and the position nearer is called perigee. what are the speeds of the two objects

Expert's answer

Objects in the elliptical orbit the position farther from the gravity source is called the apogee and the position nearer is called perigee. What are the speeds of the two objects

Solution

Using the laws of conservation of energy and angular momentum (index aa related to object in apogee, index pp related to object in apogee,)


mrava=mrpvpm r _ {a} v _ {a} = m r _ {p} v _ {p}va=rpvprav _ {a} = \frac {r _ {p} v _ {p}}{r _ {a}}mva22GmMra=mvp22GmMrpm \frac {v _ {a} ^ {2}}{2} - G \frac {m M}{r _ {a}} = m \frac {v _ {p} ^ {2}}{2} - G \frac {m M}{r _ {p}}(vp)2(rpvpra)2=2GM(1rp1ra)\left(v _ {p}\right) ^ {2} - \left(\frac {r _ {p} v _ {p}}{r _ {a}}\right) ^ {2} = 2 G M \left(\frac {1}{r _ {p}} - \frac {1}{r _ {a}}\right)vp=GM(1rp1ra)ra2ra2rp2=GMrarp2ra+rpv _ {p} = \sqrt {G M \left(\frac {1}{r _ {p}} - \frac {1}{r _ {a}}\right) \frac {r _ {a} ^ {2}}{r _ {a} ^ {2} - r _ {p} ^ {2}}} = \sqrt {G M \frac {r _ {a}}{r _ {p}} \frac {2}{r _ {a} + r _ {p}}}


Using the definition of distance between source of gravity and object in apogee and perigee (aa is semi-major axis).


ra=a(1+ε)r _ {a} = a (1 + \varepsilon)rp=a(1ε)r _ {p} = a (1 - \varepsilon)\Rightarrowvp=GM1a1+ε1εv _ {p} = \sqrt {G M \frac {1}{a} \frac {1 + \varepsilon}{1 - \varepsilon}}va=GM1a1ε1+εv _ {a} = \sqrt {G M \frac {1}{a} \frac {1 - \varepsilon}{1 + \varepsilon}}


Answer:


vp=GM1a1+ε1εv _ {p} = \sqrt {G M \frac {1}{a} \frac {1 + \varepsilon}{1 - \varepsilon}}va=GM1a1ε1+εv _ {a} = \sqrt {G M \frac {1}{a} \frac {1 - \varepsilon}{1 + \varepsilon}}

Need a fast expert's response?

Submit order

and get a quick answer at the best price

for any assignment or question with DETAILED EXPLANATIONS!

LATEST TUTORIALS
APPROVED BY CLIENTS