3.2.21 · D4Orbital Mechanics & Astrodynamics

Exercises — Bi-elliptic transfer — when it wins over Hohmann

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The vocabulary this page assumes — build it before you use it

Everything below rests on three named radii and the vis-viva equation. Let us earn each one with a picture before a single exercise.

Figure — Bi-elliptic transfer — when it wins over Hohmann

The two circular-orbit landmarks we reuse constantly (set above, since a circle has ):


Level 1 — Recognition

Exercise 1.1

A bi-elliptic transfer moves a spacecraft between two coplanar circular orbits. How many impulsive burns and how many transfer ellipses does it use, and at what radii do the burns happen?

Recall Solution
  • Three burns, two ellipses.
  • Burn 1 at (raise apoapsis to ), Burn 2 at (raise the opposite apsis from up to ), Burn 3 at (circularize).
  • Contrast with Hohmann transfer: two burns, one ellipse.

Exercise 1.2

In a bi-elliptic transfer with and , someone proposes . What is wrong with this choice?

Recall Solution

The intermediate radius must satisfy (recall is the overshoot apoapsis defined above). Here , which is geometrically impossible: the first ellipse's apoapsis has to be beyond the target so the second ellipse can "coast back down" to . If it is not a bi-elliptic transfer at all (at it degenerates to Hohmann).

Exercise 1.3

The parent note quotes two "magic numbers," and , where . State in words what each threshold guarantees.

Recall Solution
  • : Hohmann always wins — no choice of lets bi-elliptic beat it.
  • : bi-elliptic wins provided is chosen large enough.
  • : it depends on (grey zone).

Level 2 — Application

Exercise 2.1

For , compute the two circular speeds and .

Recall Solution
  • .
  • . Why this formula? It is vis-viva with (a circle), so the two energy terms leave only . What it means: the outer orbit is slow — that slowness is the resource bi-elliptic exploits.

Exercise 2.2

With , find the semi-major axis of the first transfer ellipse, then compute Burn 1, the speed change at to enter that ellipse.

Recall Solution
  • . Why: is this ellipse's periapsis, its apoapsis; average them.
  • Speed on ellipse 1 at : vis-viva with : . Why here: Burn 1 fires at , so we evaluate the new orbit's speed at .
  • Subtract circular speed: . Why subtract? We were already moving at in a circle; the burn only pays for the extra speed needed to stretch the orbit outward — a pure prograde kick, same direction, so the cost is the gap.

Exercise 2.3

At the far point , the spacecraft is on ellipse 1 () and must transfer to ellipse 2 with . Compute Burn 2 and comment on its size. Refer to the figure.

Recall Solution
  • . Why: ellipse 2 has apoapsis and periapsis ; average them.
  • Speed on ellipse 2 at (vis-viva, ): .
  • Speed on ellipse 1 at (): .
  • . Read the figure below: both speeds are prograde arrows at the far point, and both share the same dominant term — so the arrows are nearly equal length and you pay only the small orange gap between them, not their sum. This tiny far-out cost is the entire reason bi-elliptic can win.
Figure — Bi-elliptic transfer — when it wins over Hohmann

Level 3 — Analysis

Exercise 3.1

Finish Example 1 from the parent note (): compute Burn 3 and the total bi-elliptic , and confirm which side of the threshold you are on.

Recall Solution
  • (from 2.3). Where and why Burn 3 fires: at , which is the periapsis of ellipse 2, so the craft arrives moving faster than a circle there — vis-viva at : .
  • Target circular speed: .
  • — a brake (retro): you are above circular speed, so you must slow down to circularize. Take the magnitude.
  • Total: .
  • Intuition tie-back: the three burns are "climb out" (0.407) + "cheap far-out reshape" (0.044) + "gentle brake in" (0.065). The tiny middle term is the whole trick. Since , bi-elliptic should win — and the parent's Hohmann confirms it. ✅

Exercise 3.2

For the same but now , recompute the total bi-elliptic . Is a smaller better or worse here?

Recall Solution
  • , . Why: same "average the apsides" rule with the new .
  • Burn 1 (at , enter ellipse 1): .
  • Burn 2 (at , ellipse 1→2): .
  • Burn 3 (brake at ): .
  • Total: .
  • Interpretation: compared to 's , this is slightly worse. The far point at is not as slow, so Burn 2 is bigger (0.068 vs 0.044). Larger pushed the total down — the trend continues toward the bi-parabolic floor.

Exercise 3.3

Explain, using vis-viva, why increasing lowers Burn 2 but raises Burn 1, and why the net total still fell between Ex 3.2 and 3.1.

Recall Solution
  • Burn 2 ↓ (physical reason): it fires at . In vis-viva the term as for both ellipse speeds, so both roots shrink toward zero and their difference vanishes. Farther out = slower everything = cheaper reshape. This is the far-out "calm zone" of the parent's merry-go-round analogy.
  • Burn 1 ↑ (physical reason): at the ellipse-1 speed is with . As , , so this speed escape speed. Flinging farther out demands a bigger initial kick.
  • Net: going , the Burn-2 saving (plus the Burn-3 shift) outweighed the Burn-1 rise, so the total dropped . The two effects are a tug-of-war that only stops improving at the bi-parabolic limit.

Level 4 — Synthesis

Exercise 4.1

For (), the parent found Hohmann and bi-elliptic () . Reproduce the bi-elliptic total to full precision and identify which single burn is responsible for bi-elliptic losing.

Recall Solution
  • .
  • Burn 1: — identical to Ex 2.2, because Burn 1 depends only on and , not on .
  • Burn 2: .
  • Burn 3 (brake at ): .
  • Total: .
  • On the parent's : that value used the rounded intermediate roots (e.g. , printed as ) and accumulated those roundings; carrying full precision the honest total is . The gap is not trivial rounding of the final answer — it is the compounded effect of rounding each square root to 4 digits before subtracting nearly-equal numbers (catastrophic cancellation in Burn 2 especially). Either way the conclusion stands: , Hohmann wins.
  • Culprit: Burn 1 (). At small you still pay the full escape-like cost of flinging out to , but the target sits at only — that huge climb is mostly wasted, and the meagre Burn-2 saving cannot repay it. → Hohmann wins.

Exercise 4.2

A mission planner has and target (inside the grey zone ). They try . Does bi-elliptic beat Hohmann here? Compute both.

Recall Solution

Hohmann, :

  • Burn A: . Why: vis-viva at on the Hohmann ellipse, minus .
  • Burn B: . Why: Hohmann arrives at below circular speed (it's apoapsis), so this burn adds speed.
  • Hohmann total .

Bi-elliptic, : :

  • Burn 1: .
  • Burn 2: .
  • Burn 3 (brake): .
  • Bi-elliptic total .

Result: bi-elliptic wins, but barely (). This is the grey zone: the outcome hinges on and the margin is razor-thin. A planner weighs that sliver against a far longer flight time.


Level 5 — Mastery

Exercise 5.1

Derive the bi-parabolic () limit of the total in normalized units (), as a function of with . Then evaluate it at and compare to Ex 3.1's finite result.

Recall Solution

Take limits term by term (with ), each with its physical meaning.

  • Burn 1 (the climb): , so . Thus — you reach escape speed at and no more.
  • Burn 2 (far-out reshape): both speeds at scale like ; their difference . So — free plane/apsis reshape at infinity.
  • Burn 3 (brake in): , so . Thus — the same escape-vs-circular gap, scaled down by the slower speeds at . At : . Compare Ex 3.1's finite value — the bi-parabolic limit is lower (it is the floor), confirming larger keeps helping toward this bound.

Exercise 5.2

Using the bi-parabolic formula from 5.1 and the exact Hohmann formula, verify the lower crossover by checking that at the bi-parabolic total is just about equal to Hohmann, and that for Hohmann is strictly cheaper (test ).

Recall Solution

Hohmann in normalized units, (derived the same way as Ex 4.2, now symbolic): At : .

  • Burn A: .
  • Burn B: .
  • .
  • Bi-parabolic: .
  • equal to rounding. ✅ This equality is precisely why is the lower magic number: below it the bi-parabolic (best-possible bi-elliptic) can no longer match Hohmann.

At (below threshold):

  • Hohmann: ; Burn A ; Burn B ; total .
  • Bi-parabolic: .
  • Hohmann strictly wins, as promised for . ✅

Exercise 5.3 (Open synthesis)

The parent note says bi-elliptic makes plane changes cheap "far out." Using vis-viva intuition and Plane change maneuvers, argue qualitatively why performing a combined plane-change + apsis-raise at can beat doing the plane change at — and state the one-line rule.

Recall Solution

A pure plane change of angle at speed costs — it is proportional to the speed at the burn point (see Plane change maneuvers). At the spacecraft is fast ( large), so rotating the orbit plane is expensive. At the speed is tiny (vis-viva: as ), so the same angular rotation costs almost nothing.

  • The rule: rotate where you are slow. Fling out to , do the plane change (and periapsis raise) at that lazy far point, then coast back. When the required plane change is large, this can save more than the extra climbs cost — a direct cousin of the size-change crossover, and the inverse of the Oberth effect (which says speed changes are cheap where you are fast).

Flashcards

Bi-parabolic () total in units ?
.
Which single burn makes bi-elliptic lose at small ?
Burn 1 — you pay the full escape-like cost of flinging out to even though the target is close.
A plane change costs what?
The speed at the burn point — so rotate where you are slow (far out).
As increases, Burn 1 does what, and Burn 2 does what?
Burn 1 rises toward escape speed; Burn 2 falls toward zero.
What is for an ellipse in terms of its apsides?
— half the longest diameter.