Find Speed Changes for Spacecraft Orbit Transfer: Mplanet/MEarth = 0.75

Click For Summary
SUMMARY

The discussion focuses on calculating speed changes for a spacecraft transitioning between elliptical orbits JK and MN, with intermediate adjustments to a circular orbit KL. The mass ratio of the planet to Earth is Mplanet/MEarth = 0.75, and the planet's radius is Rplanet = 3000 mi. Key issues identified include the incorrect mixing of miles and metric units in calculations and a misunderstanding of the orbital radius variable in velocity formulas. Participants emphasize the need for a thorough revision of calculations to ensure accuracy.

PREREQUISITES
  • Understanding of orbital mechanics and elliptical orbits
  • Familiarity with velocity calculations in astrophysics
  • Knowledge of unit conversions between imperial and metric systems
  • Proficiency in using orbital equations for spacecraft navigation
NEXT STEPS
  • Review the principles of orbital mechanics, focusing on elliptical and circular orbits
  • Study the correct application of velocity formulas in orbital dynamics
  • Learn about unit conversion techniques for consistent calculations
  • Explore simulation tools for spacecraft trajectory planning, such as GMAT or STK
USEFUL FOR

Aerospace engineers, astrophysicists, and students studying orbital mechanics who are involved in spacecraft trajectory analysis and optimization.

Faraz
Messages
16
Reaction score
0
Question
A spacecraft starts in elliptical orbit JK (red solid curve) around some planet and transfers to elliptical orbit MN (blue solid curve). To do so, it changes its speed at Kand inserts into the circular orbit KL (dashed green curve). At L, it changes speed again to insert into elliptical orbit LM (dashed magenta curve). Finally, at M, it changes speed to insert into the final orbit MN. Find all the changes in speed. Mass of planet compared to mass of Earth: Mplanet /MEarth = 0.75 Radius of planet: Rplanet = 3000 mi a = 400 mi b = 1200 mi c = 300 mi d = 1000 mi

Homework Equations


I just want to make sure I did it correctly before submitting my answer (ATTACHED)

The Attempt at a Solution

 

Attachments

  • media-ab8-ab8cb35e-ec6e-4c70-a40c-eaf60ede7971-phpvvLt0m.png
    media-ab8-ab8cb35e-ec6e-4c70-a40c-eaf60ede7971-phpvvLt0m.png
    49.8 KB · Views: 432
  • media-bd2-bd212ea0-1983-4516-8459-4e07a92beda7-phpFeby6F.png
    media-bd2-bd212ea0-1983-4516-8459-4e07a92beda7-phpFeby6F.png
    13.2 KB · Views: 440
  • media-279-279ab89c-245f-483b-812e-69e47cc2dce7-phpoJR0Pz.png
    media-279-279ab89c-245f-483b-812e-69e47cc2dce7-phpoJR0Pz.png
    21.9 KB · Views: 404
  • media-1da-1da7f9b6-1739-4b49-b930-4fd1acd8725b-phpOZdIiM.png
    media-1da-1da7f9b6-1739-4b49-b930-4fd1acd8725b-phpOZdIiM.png
    23 KB · Views: 386
Last edited by a moderator:
Physics news on Phys.org
Faraz said:
Question
A spacecraft starts in elliptical orbit JK (red solid curve) around some planet and transfers to elliptical orbit MN (blue solid curve). To do so, it changes its speed at Kand inserts into the circular orbit KL (dashed green curve). At L, it changes speed again to insert into elliptical orbit LM (dashed magenta curve). Finally, at M, it changes speed to insert into the final orbit MN. Find all the changes in speed. Mass of planet compared to mass of Earth: Mplanet /MEarth = 0.75 Radius of planet: Rplanet = 3000 mi a = 400 mi b = 1200 mi c = 300 mi d = 1000 mi

Homework Equations


I just want to make sure I did it correctly before submitting my answer (ATTACHED)

The Attempt at a Solution

Your calculations need total revision.

You've mixed miles and the metric system in you calculations and produced some really strange results.
 
...Also note that in your formula for velocity, the r variable is the value of the orbit radius at the point of interest, not the radius of the planet.
 

Similar threads

  • · Replies 2 ·
Replies
2
Views
5K