How to find the transfer orbit from a initial circular orbit to a final elliptical orbitHow to calculate delta-v required for a planet-to-planet Hohmann transfer?Transfer between elliptical orbitsOptimum delta-v burn to change periapsis or apoapsis at an arbitrary point on an elliptical orbit?How much delta v does it take to get to the Sun-Earth Lagrange 3 point?How can I control the departure and arrival aiming radii in an ideal interplanetary trajectory?Would a Mars flyby be possible on a transfer orbit from Saturn's moon of Titan to Earth?How to intuitively explain that tri-elliptic transfers are not better than bi-elliptic transfers?Elliptical orbits transformed to “equivalent” circular orbitWhy is a Hohmann transfer from an elliptical orbit to a circular one more efficient if done from Perigee?How can I change plane (inclination and OMEGA) during a bielliptical transfer?
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How to find the transfer orbit from a initial circular orbit to a final elliptical orbit
How to calculate delta-v required for a planet-to-planet Hohmann transfer?Transfer between elliptical orbitsOptimum delta-v burn to change periapsis or apoapsis at an arbitrary point on an elliptical orbit?How much delta v does it take to get to the Sun-Earth Lagrange 3 point?How can I control the departure and arrival aiming radii in an ideal interplanetary trajectory?Would a Mars flyby be possible on a transfer orbit from Saturn's moon of Titan to Earth?How to intuitively explain that tri-elliptic transfers are not better than bi-elliptic transfers?Elliptical orbits transformed to “equivalent” circular orbitWhy is a Hohmann transfer from an elliptical orbit to a circular one more efficient if done from Perigee?How can I change plane (inclination and OMEGA) during a bielliptical transfer?
$begingroup$
Is a hohmann transfer or bi-elliptical transfer more efficient for this case? How can I find the transfer orbit that conserves the most deltaV?
I will be going from a circular Earth centered orbit to an elliptical sun centered orbit. Assuming the orbits are coplanar.
orbital-mechanics orbital-maneuver hohmann-transfer
asked 5 hours ago
FreddyFreddy
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add a comment |
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Is a hohmann transfer or bi-elliptical transfer more efficient for this case? How can I find the transfer orbit that conserves the most deltaV?
I will be going from a circular Earth centered orbit to an elliptical sun centered orbit. Assuming the orbits are coplanar.
orbital-mechanics orbital-maneuver hohmann-transfer
asked 5 hours ago
FreddyFreddy
61
New contributor
Freddy is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
Check out our Code of Conduct.
$endgroup$
add a comment |
$begingroup$
Is a hohmann transfer or bi-elliptical transfer more efficient for this case? How can I find the transfer orbit that conserves the most deltaV?
I will be going from a circular Earth centered orbit to an elliptical sun centered orbit. Assuming the orbits are coplanar.
orbital-mechanics orbital-maneuver hohmann-transfer
asked 5 hours ago
FreddyFreddy
61
New contributor
Freddy is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
Check out our Code of Conduct.
$endgroup$
Is a hohmann transfer or bi-elliptical transfer more efficient for this case? How can I find the transfer orbit that conserves the most deltaV?
I will be going from a circular Earth centered orbit to an elliptical sun centered orbit. Assuming the orbits are coplanar.
orbital-mechanics orbital-maneuver hohmann-transfer
orbital-mechanics orbital-maneuver hohmann-transfer
asked 5 hours ago
FreddyFreddy
61
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asked 5 hours ago
FreddyFreddy
61
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asked 5 hours ago
FreddyFreddy
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asked 5 hours ago
FreddyFreddy
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asked 5 hours ago
FreddyFreddy
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The semi-major axis and eccentricity of your target orbit will determine whether a Hohmann transfer (i.e. bi-impulse transfer) or bi-elliptic transfer (i.e. tri-impulse transfer) is more $Delta$V efficient.
Here is a paper that explains the equations governing this problem.
answered 4 hours ago
OctogonOctogon
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not sure if it is just me but the article listed has a lot of the equations with symbols that didnt transfer properly so it looks like gibberish in some places
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– Freddy
3 hours ago
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1 Answer
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1 Answer
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$begingroup$
The semi-major axis and eccentricity of your target orbit will determine whether a Hohmann transfer (i.e. bi-impulse transfer) or bi-elliptic transfer (i.e. tri-impulse transfer) is more $Delta$V efficient.
Here is a paper that explains the equations governing this problem.
answered 4 hours ago
OctogonOctogon
211
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Octogon is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
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$endgroup$
$begingroup$
not sure if it is just me but the article listed has a lot of the equations with symbols that didnt transfer properly so it looks like gibberish in some places
$endgroup$
– Freddy
3 hours ago
add a comment |
$begingroup$
The semi-major axis and eccentricity of your target orbit will determine whether a Hohmann transfer (i.e. bi-impulse transfer) or bi-elliptic transfer (i.e. tri-impulse transfer) is more $Delta$V efficient.
Here is a paper that explains the equations governing this problem.
answered 4 hours ago
OctogonOctogon
211
New contributor
Octogon is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
Check out our Code of Conduct.
$endgroup$
$begingroup$
not sure if it is just me but the article listed has a lot of the equations with symbols that didnt transfer properly so it looks like gibberish in some places
$endgroup$
– Freddy
3 hours ago
add a comment |
$begingroup$
The semi-major axis and eccentricity of your target orbit will determine whether a Hohmann transfer (i.e. bi-impulse transfer) or bi-elliptic transfer (i.e. tri-impulse transfer) is more $Delta$V efficient.
Here is a paper that explains the equations governing this problem.
answered 4 hours ago
OctogonOctogon
211
New contributor
Octogon is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
Check out our Code of Conduct.
$endgroup$
The semi-major axis and eccentricity of your target orbit will determine whether a Hohmann transfer (i.e. bi-impulse transfer) or bi-elliptic transfer (i.e. tri-impulse transfer) is more $Delta$V efficient.
Here is a paper that explains the equations governing this problem.
answered 4 hours ago
OctogonOctogon
211
New contributor
Octogon is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
Check out our Code of Conduct.
answered 4 hours ago
OctogonOctogon
211
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answered 4 hours ago
OctogonOctogon
211
answered 4 hours ago
OctogonOctogon
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211
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$begingroup$
not sure if it is just me but the article listed has a lot of the equations with symbols that didnt transfer properly so it looks like gibberish in some places
$endgroup$
– Freddy
3 hours ago
add a comment |
$begingroup$
not sure if it is just me but the article listed has a lot of the equations with symbols that didnt transfer properly so it looks like gibberish in some places
$endgroup$
– Freddy
3 hours ago
$begingroup$
not sure if it is just me but the article listed has a lot of the equations with symbols that didnt transfer properly so it looks like gibberish in some places
$endgroup$
– Freddy
3 hours ago
$begingroup$
not sure if it is just me but the article listed has a lot of the equations with symbols that didnt transfer properly so it looks like gibberish in some places
$endgroup$
– Freddy
3 hours ago
add a comment |
Freddy is a new contributor. Be nice, and check out our Code of Conduct.
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