Circular orbit VS Elliptical orbit? Differences?

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SUMMARY

The discussion focuses on the conditions required for man-made satellites to achieve circular and elliptical orbits around the Earth. For a circular orbit, a satellite must be launched with a tangential speed of 8 km/s (option B) and can be launched horizontally at a distance over 150 km above the Earth (option D). In contrast, for an elliptical orbit, the satellite must be launched with a tangential speed greater than 8 km/s (option C) and can also be launched horizontally at a distance over 150 km above the Earth (option D). The conversation also touches on the theory of relativity, specifically regarding time dilation experienced by astronauts traveling at near-light speed.

PREREQUISITES
  • Understanding of orbital mechanics
  • Knowledge of tangential speed and its role in satellite motion
  • Familiarity with the concept of inertial reference frames
  • Basic principles of the theory of relativity
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  • Research the physics of orbital mechanics and satellite dynamics
  • Learn about the calculations for achieving stable circular orbits
  • Study the effects of velocity on satellite trajectories, focusing on elliptical orbits
  • Explore the implications of the theory of relativity on time dilation for astronauts
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Aerospace engineers, physics students, satellite communication professionals, and anyone interested in the mechanics of satellite orbits and the theory of relativity.

graphicer89
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Circular orbit VS Elliptical orbit?? Differences?

Homework Statement


Hi I am trying to understand some questions about Space and man made satellites...i would really appreciate it if someone could help me out thanks...also i included an extra question about the theory of relativity if you can help me out i would appreciate it...


6) What conditions must be met if a man made satellite is to attain a CIRCULAR ORBIT around the earth? ( choose as many as apply)
A) It must be launched with a tangential speed of 0
B) It must be launched with a tangential speed of 8 km/s
C) It must be launched with a tangential speed greater than 8 km/s
D)It must be launched horizontally at a distance over 150 km above the Earth
E) It must be launched vertically with a speed of 8 km/s

4) What conditions must be met if a man made satellite is to attain an ELLIPTICAL ORBIT around the earth? (choose as many as apply)
A) It must be launched with a tangential speed of 0
B) It must be launched with a tangential speed of 8 km/s
C) It must be launched with a tangential speed greater than 8 km/s
D)It must be launched horizontally at a distance over 150 km above the Earth
E) It must be launched vertically with a speed of 8 km/s


Belinda takes a trip in a rocket ship that travels at near light speed of her twin Melinda stays at home. Which of the following statements is true?
A) When Belinda arrives back at earth, Melinda will be much older than Belinda because from Belindas frame of reference on the rocket,time in Melindas frame of reference was passing slowly.
B) When Belinda arrives back on Earth Melinda will be much older than Belinda because Belindas frame of reference on the rocket is not an inertial reference frame.
 
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Welcome to PF!

Hi graphicer89! Welcome to PF! :wink:

Show us what you think (with reasons), and where you're stuck, and then we'll know how to help! :smile:
 


Well the questions about Belinda i think its A because Belinda (THe one who went to space ) her traveling at the speed of light made time for her to pass slowly but i am not sure though...the INERTIAL REFERENCE FRAME on the second one throws me offf...but talking about the first 2 i think the 6 i think is B and E because it falls around the Earth so it has to be less than 11. ? of the escape speed...and number 4 i think C and D because that one is like an oval ..it rotates around the Earth and keeps going pass the earth...but what do you think??
 

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