Intuition The one core idea
Sending a spacecraft from Earth to Mars is really a tangle of everything pulling on everything , which nobody can solve with a clean formula. So we cheat: at each moment we pretend only the nearest heavy body matters , solve that easy one-body problem, and glue the easy pieces together — hyperbola near a planet, ellipse around the Sun.
Before you can read the parent note on the patched conic method , you need every symbol it throws at you to already feel obvious. This page builds each one from nothing, in an order where each idea leans on the one before it.
The central body is the single heavy object we pretend is doing all the pulling at a given moment. Picture a lamppost with a ball on a string swinging around it — the lamppost is the central body, the ball is our spacecraft.
Definition Conic (conic section)
A conic is any curve you get by slicing a cone with a flat plane: circle, ellipse, parabola, hyperbola. In gravity, an object around a single central body always traces one of these. That is why the method is called "patched conic ": each easy piece is one of these curves.
Look at the figure: same cone, four slices, four curves. A closed slice (ellipse) means the object is bound and comes back around. An open slice (hyperbola) means it flies off forever. The whole trip uses one ellipse (the Sun-bound cruise) glued to two hyperbolas (the fly-away/fly-in near each planet). Keep that mental image — every symbol below decorates one of these curves.
r = distance from the central body
r is simply how far the spacecraft is from the centre of the body doing the pulling , measured in metres. On a picture it is the length of the straight arrow from the central body to the spacecraft.
Gravity gets weaker with distance. Every gravity formula asks "how far away?" first — so r is the input to almost everything. Notice the same letter means distance from the Sun in the cruise chapter but distance from the planet in the fly-by chapter. Whenever you see r , first ask: distance from what?
a = semi-major axis
An ellipse is a stretched circle. Its longest line, corner to corner through the centre, is the major axis . Half of that is the semi-major axis a . It is the single number that says "how big is this orbit."
Definition Perihelion & aphelion (perigee & apogee)
On the transfer ellipse the closest point to the Sun is perihelion (radius r 1 in the note) and the farthest is aphelion (radius r 2 ). "Peri-" = near, "apo-" = far, "-helion" = Sun, "-gee" = Earth.
Because the two extreme points sit on opposite ends of the major axis,
a t = 2 r 1 + r 2 .
What this says: the semi-major axis of the trip ellipse is just the average of the near and far distances. Look at the figure — r 1 and r 2 are the two ends, their midpoint is the centre, and a t reaches from centre to end.
Subscripts you will meet: a p = a p lanet's orbit size (its distance from the Sun), a t = the t ransfer ellipse's size.
m p = mass of a p lanet, m ⊙ = mass of the Sun (the little circle-with-dot ⊙ is the ancient symbol for the Sun), m E = mass of E arth. Mass is "how much stuff," and more stuff means stronger pull.
G — the gravitational constant
G is nature's fixed conversion factor turning "mass and distance" into "pull." It never changes: G = 6.674 × 1 0 − 11 in SI units.
v = speed
v is how fast the spacecraft moves, in metres per second. On a picture it is an arrow along the direction of motion; its length is the speed.
The parent note names several speeds — they are all just v measured at a particular place or relative to a particular body:
Symbol
Plain meaning
v c
speed to hold a c ircular orbit at some radius
v esc
esc ape speed — just barely enough to leave forever
v p
speed at p erigee (closest approach)
v ∞
leftover speed infinitely far away, after climbing out
v t
speed on the t ransfer ellipse
Intuition The star of the show:
v ∞
Read v ∞ as "vee-infinity" — the speed the spacecraft still has left over once it has climbed completely out of a planet's gravity well, measured relative to that planet . Picture throwing a ball straight up: escape speed gets it to the top with nothing left; extra speed means it's still moving at the top — that leftover is v ∞ . This one symbol is the "handshake" that glues the fly-away hyperbola to the Sun-cruise ellipse.
Definition Specific energy
ε
"Specific" means per kilogram , so we don't carry the spacecraft's mass around. The energy of an orbit has two parts:
ε = motion (kinetic) 2 v 2 − depth in the well (potential) r μ .
Intuition Picture the gravity well
Imagine a smooth funnel: deep near the central body, flat far away. The − μ / r term is how deep you are (negative = down in the funnel). The v 2 /2 term is your speed. Their sum stays constant as you coast — trade depth for speed and back, like a skateboarder in a bowl.
ε < 0 : trapped in the funnel → ellipse (comes back).
ε = 0 : exactly escapes → parabola .
ε > 0 : escapes with speed to spare → hyperbola , and that spare speed is exactly v ∞ , because far away (r → ∞ ) the depth term vanishes and ε = 2 1 v ∞ 2 .
This single conserved quantity is why the vis-viva formula (next) exists, and why burning deep in the well is cheap.
Two useful special cases fall straight out:
Circle (r = a ): v c = μ / r .
Escape (a → ∞ , so 1/ a → 0 ): v esc = 2 μ / r — the 2 is why escape speed is 2 × circular speed.
Definition Exponents you must read fluently
r 2 means r × r ; r 3 means r × r × r .
A square root x asks "what number times itself gives x ?" — it undoes squaring, which is why solving v 2 = … for v needs a root.
A fractional power x 2/5 means "take the fifth root, then square" (or square then fifth-root — same thing). It appears in the SOI radius because a r 5 = … equation is undone by the 1/5 power.
2/5 is nothing to fear
The parent's derivation ends at r 5 = a p 5 ( m p / m ⊙ ) 2 . To free r , take the fifth root of both sides: the 5 on the left cancels, and the ( m p / m ⊙ ) 2 becomes ( m p / m ⊙ ) 2/5 . That's all the mysterious 2/5 is — the fifth root of a squared ratio.
π and the half-orbit time
π ≈ 3.14159 is the ratio of a circle's edge to its diameter. Orbital periods carry it because going "all the way around" is a full turn. The parent's transfer time
t = π a t 3 / μ ⊙
is half of a full elliptical period T = 2 π a 3 / μ — the 2 dropped to a bare π because a Hohmann transfer is exactly half a lap. That period formula is Kepler's third law in disguise.
Δ v ("delta-vee")
The Greek Δ (capital delta) means change in . So Δ v is the change in speed an engine burn produces. It is the true "cost" of a manoeuvre — more Δ v needs more fuel.
Δ v = v after − v before .
The departure burn costs Δ v = v p − v c i r c : raise your circular speed up to the hyperbola's perigee speed.
gravitational parameter mu
heliocentric transfer ellipse
sphere of influence radius
Each foundation box is one symbol you just learned; the arrows show which parent-note result it powers.
Once these symbols feel automatic, the parent leans directly on: Sphere of influence , Hohmann transfer orbit , Hyperbolic escape trajectories , the Oberth effect , and timing via Launch windows & synodic period .
Cover the answers; you are ready when each is instant.
μ means... ::: G times the central body's mass — the "pulling strength," used so we don't carry G and M separately.
r always demands one question first, namely... ::: "distance from which body?" (Sun in the cruise, planet in the fly-by).
The semi-major axis of a Hohmann transfer is... ::: a t = ( r 1 + r 2 ) /2 , the average of the near and far distances.
Specific orbital energy has two parts... ::: kinetic v 2 /2 minus potential μ / r ; their sum is constant along a coast.
ε < 0 , = 0 , > 0 give which curves... ::: ellipse, parabola, hyperbola respectively.
v ∞ is the speed... ::: left over infinitely far from a planet, measured relative to that planet .
The vis-viva equation is... ::: v = μ ( 2/ r − 1/ a ) .
Escape speed relates to circular speed by a factor... ::: 2 (escape = 2 μ / r , circular = μ / r ).
x 2/5 means... ::: take the fifth root and square (undoes an r 5 equation).
Δ v means... ::: change in speed from a burn — the fuel "cost" of a manoeuvre.
Half an elliptical period is... ::: t = π a 3 / μ (full period drops its factor of 2 ).