Editing 3189: Conic Sections

{{comic
| number    = 3189
| date      = January 2, 2026
| title     = Conic Sections
| image     = conic_sections_2x.png
| imagesize = 288x322px
| noexpand  = true
| titletext = They're not generally used for crewed spacecraft because astronauts HATE going around the corners.
}}

==Explanation==
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A {{w|Kepler orbit}} describes the simplified motion of one celestial objects relative to another. Such an orbit will form a {{w|conic section}}. A conic section is a curve obtained from a cone's surface intersecting a plane. The three types of conic section are the hyperbola, the parabola, and the ellipse; the circle is a special case of the ellipse, though it was sometimes considered a fourth type. In reality, this model is based only on their basic gravitational forces and ignores any other factors such as the gravity of other objects, atmospheric drag, each object being a non-spherical(/non-point) body of non-uniform density and any {{w|Relativistic angular momentum#Orbital 3d angular_momentum|relativistic effects}}, but it serves as the basis for most orbital calculations before further refining with the most relevant additional perturbations.

[[File:TypesOfConicSections.jpg|thumb|alt=Example conic sections|How conic sections emerge from various planar intersections with bidirectional cones, which technically continue beyond the 'top' and 'bottom' of each diagram.]]

In real conic sections, the cone extends to infinity. In the comic, however, the "conic section" representing the satellite's orbit has been assumed to have a base at a distance that inconveniently crosses the indicated orbital path (that might be assumed to be eliptical, otherwise), resulting in sharp corners where the angled planar section through the cone meets that base. As alluded to in the title text, these corners would be extremely uncomfortable for an astronaut in a crewed spacecraft. Such an extreme and sudden change in direction would require a very large, potentially dangerous, G-force.

Being in a free orbit necessarily means following an ellipse (or very similar, outside of the mathematically strict {{w|two-body problem}}) in which there is net zero acceleration, combining the pull of gravity and the forces that would be felt due to the continually changing direction alone. Being forced off this ellipse to move across the totally imaginary and arbitrary conic-base would force an instantaneous acute change of direction for no other reason than to follow the imperfectly understood mathematical 'model' at two arbitrary points (reaching the baseline and rejoining the true curve again), which would technically require infinite acceleration each time.

Alternately, deliberately 'cutting the corner' of an orbit would require the best effort of the spacecraft to stick to the truncated-orbital path, requiring as much {{w|Delta-v|thrust}} by the craft as it can muster (which any occupants would have to endure), including along the less uncomfortable but still forceful passage along the 'straight' bit of the orbit through the curved space-time of the {{w|gravitational field}} of the parent body. We also aren't given any indication of how the 'radial' velocity might be intended to change during the 'flat' phase, such as if it obeys the same {{w|Kepler's laws of planetary motion#Second law|constant 'area sweeping' rule}} as for the elliptic part of the path.

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==Transcript==
{{incomplete transcript|Don't remove this notice too soon.}}
:[A view of the Earth, focused on Asia and the Indian Ocean with East Africa at left and the Western Pacific and Australia at right. A satellite is shown in an unusual orbit around the planet.]
:[Caption below the panel:]
:All Keplerian orbits are conic sections. For example, this one uses the base of the cone.
{{comic discussion}}<noinclude>

[[Category:Space]]
[[Category:Geometry]]