Intuition The one core idea
An orbit is a speed–distance bargain : the farther you are from the planet, the slower you must go, and this trade is fixed once you know the orbit's size . A Hohmann transfer just links two circular bargains with a single stretched loop, paying the smallest possible "speed change" toll at each end.
Everything in the parent note rests on a handful of symbols. Below, each one is built from nothing: plain words → the picture → why the topic needs it. Read top to bottom; nothing is used before it is born.
M — the mass you orbit
M is the mass of the big object in the middle (Earth, the Sun). Picture a heavy bowling ball sitting on a stretched rubber sheet: it makes a dip. Everything else rolls around that dip.
G — the gravitational constant
G is nature's fixed "strength dial" for gravity, the same number everywhere in the universe: G ≈ 6.674 × 1 0 − 11 m 3 kg − 1 s − 2 . It converts mass into pull .
Why bundle them? In every orbit formula G and M appear glued together, always as the product GM . So we give the pair one name:
μ (mu) — the gravitational parameter
μ = GM
One number that says "how strongly this particular central body bends paths." For Earth, μ ⊕ = 3.986 × 1 0 5 km 3 / s 2 .
Why the topic needs it: every speed and every burn in the derivation is a formula with μ in it. It is the single knob describing the planet's gravity.
r — distance from the centre
r is the straight-line distance from the centre of the planet to the spacecraft — not from the ground, from the centre . Picture a string tied to the planet's core; r is its length right now.
Why "from the centre"? Gravity acts as if all of M sits at the central point, so distances are measured to that point. This is why a "7000 km" orbit around Earth (radius ≈ 6371 km) is only ∼ 629 km above the surface.
Common mistake Confusing altitude with
r
Feels right: "I'm 600 km up, so r = 600 ." Fix: r = R planet + altitude . Always measure to the centre.
r 1 and r 2 — inner and outer circle radii
r 1 = radius of the small starting circle. r 2 = radius of the big target circle. In the parent's example r 1 = 7000 km, r 2 = 42164 km.
Now the shape that connects them:
A "stretched circle" — an oval. Where a circle has one centre-distance, an ellipse has a closest point and a farthest point from the planet.
Definition Periapsis and apoapsis
Periapsis = the closest point of the ellipse to the planet (here it sits at r 1 ).
Apoapsis = the farthest point (here it sits at r 2 ).
Look at the figure: the transfer ellipse kisses the inner circle at periapsis and the outer circle at apoapsis. That double-kiss is the whole Hohmann idea.
a — semi-major axis
a is half the longest diameter of an ellipse — the distance from the centre of the oval out to its most-stretched edge. For a circle (a special, un-stretched ellipse) a = r .
The single most useful fact about a : the closest and farthest distances add up to the full long diameter, which is 2 a :
r peri + r apo = 2 a
a is the "size" of the orbit
Two orbits with the same a carry the same total energy , even if one is a fat oval and one is a thin sliver. So a is the orbit's "energy fingerprint." That is exactly why the transfer ellipse's size is
a t = 2 r 1 + r 2
— its long diameter runs from the inner kiss (r 1 ) to the outer kiss (r 2 ).
v — orbital speed
v is how fast the spacecraft moves along its path , measured in km/s. It is a magnitude here — just "how fast," direction handled separately.
The parent uses many flavoured v 's; here is the full dictionary so no subscript ambushes you:
Symbol
Plain words
v c 1
speed on the inner circle
v c 2
speed on the outer circle
v p
speed at periapsis of the transfer ellipse
v a
speed at apoapsis of the transfer ellipse
Why (the square root)? A square root is the tool that undoes squaring. Orbital energy naturally gives us v 2 (kinetic energy uses v 2 ), so to recover the actual speed v we must take the square root of what the energy equation hands us.
This is the Vis-viva equation , the one law that ties v , r , and a together.
Intuition Read it like a sentence
r 2 : the closer you are (small r ), the bigger this term, so the faster you go — like a comet whipping around the Sun.
− a 1 : a fixed "tax" set only by the orbit's size a . A bigger orbit (large a ) has a smaller tax, but you also start slower at any given r .
Put together: near = fast, far = slow, and the size a sets the whole bargain. Every burn in the derivation is just this equation evaluated at two different r 's.
Why we need this and not just v circ ? On the ellipse , r changes as you fly, but v circ only works when r = a . Vis-viva is the general tool that gives v at any point of any orbit — see Orbital energy & semi-major axis .
Δ v (delta-vee) — change in speed
The Greek letter Δ (delta) means "the change in." So Δ v = "how much the speed changed" during an engine burn:
Δ v = v after − v before
Picture the speedometer needle jumping from one value to another; Δ v is the size of that jump.
Why it is the currency: rocket fuel maps almost directly onto Δ v (via the rocket equation, see Delta-v budget ). Less Δ v = less fuel = cheaper mission. "Minimum energy transfer" really means minimum total Δ v .
Intuition Why we can just subtract (not vector-add)
Because Hohmann burns are done tangent — the new velocity points the same direction as the old one. Two arrows on the same line: the change is simply the difference of their lengths. That is the payoff of choosing tangent burns.
Recall The full symbol table (cover the right side)
M ::: mass of the central body
G ::: universal gravitational constant
μ = GM ::: gravitational parameter of the central body
r ::: distance from the planet's centre to the craft
r 1 , r 2 ::: inner / outer circular orbit radii
a ::: semi-major axis = half the ellipse's long diameter = orbit "size"
a t ::: semi-major axis of the transfer ellipse = ( r 1 + r 2 ) /2
v ::: orbital speed (magnitude)
v circ = μ / r ::: speed to hold a circle of radius r
v p , v a ::: speeds at periapsis / apoapsis of the transfer ellipse
Δ v ::: change in speed produced by a burn (our fuel currency)
ε ::: specific orbital energy = 2 1 v 2 − μ / r
π ::: 3.14159..., appears in the transfer-time (half-orbit) formula
v_circ on the two circles
Test yourself — say the answer aloud, then reveal:
What does μ stand for and why glue G and M ? μ = GM ; they always appear together, so one symbol captures the central body's gravity strength.
Is r measured from the ground or the centre? From the centre of the planet: r = R planet + altitude .
What is a in one phrase? Half the ellipse's longest diameter — the orbit's "size" and energy fingerprint.
Why is a t = ( r 1 + r 2 ) /2 ? Periapsis at r 1 plus apoapsis at r 2 equals the long diameter 2 a t .
State vis-viva and what each term means. v 2 = μ ( 2/ r − 1/ a ) ; 2/ r = near-is-fast, − 1/ a = size-set tax.
What is v circ and when is it valid? μ / r , the speed to hold a circle — only when
r = a .
What does Δ v measure and why do we minimise it? The size of a speed jump from a burn; it maps to fuel, so least Δ v = cheapest mission.
Why can Hohmann burns be added as plain numbers? Burns are tangent, so old and new velocities are collinear — subtract magnitudes, no vectors needed.