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Libratrix
Lagrange Points / Three-Body Equilibrium Physics
Libratrix is a Pixelated Physics law character, one of our forces designs. At the L2 Lagrange point, Sun and Earth gravity balance an orbit, but the balance is unstable, so spacecraft need nudges. This is a 3" × 3" pixel-art sticker. The physics panel below gives the equation, what each symbol means and the sources.
Shipping calculated at checkout by destinationMade to order, ships in 2–5 business days
One equation · 60 seconds · one try · once a day.
Details
Size3″ × 3″
3″ × 3″ kiss-cut sticker.
Shipping
Shipping calculated at checkout by destination. Printed to order for you.
Returns & replacements21 days
Every item is printed to order, so we can’t accept returns or exchanges for change of mind, or if you ordered the wrong size or colour.
Print defect, misprint, damage or the wrong item? We’ll send a free replacement, or a refund if you prefer. Report it within 21 days of delivery with a photo; no need to send it back.
The physics
Two bodies orbiting each other have five points where a small third body can keep pace with them. For the Sun and Earth, L2 lies a little beyond Earth, and the triangular points L4 and L5 are stable only when one mass greatly outweighs the other.
Equations
| Symbol | Meaning | Unit |
|---|---|---|
| \(r_{L2}\) | distance from the smaller body to L2 (second line: Sun–Earth L2, beyond Earth) | \(\mathrm{m}\) |
| \(R\) | distance between the two bodies | \(\mathrm{m}\) |
| \(M_1, M_2\) | masses of the larger and the smaller body | \(\mathrm{kg}\) |
| \(M_1/M_2\) | mass ratio; above about 24.96, L4 and L5 are stable (Routh) | \(\mathrm{1}\) |
Sources
- Encyclopaedia Britannica — Lagrange point (Lagrange 1772; L4/L5 stability above 24.96; Trojan asteroids) (opens in a new tab)
- Routh (1874–75) On Laplace’s Three Particles, with a Supplement on the Stability of Steady Motion, Proc. London Math. Soc. s1-6, 86–97 (opens in a new tab)
- NASA Science — What is a Lagrange Point? (opens in a new tab)
- STScI JWST User Documentation — JWST Orbit (orbits around L2; station-keeping on average every 42 days) (opens in a new tab)
- NASA NTRS — Flight Dynamics Planning and Operations Support for the JWST Mission (AAS 22-611) (opens in a new tab)
- Connors, Wiegert & Veillet (2011) Earth’s Trojan asteroid, Nature 475, 481 (opens in a new tab)
- Sicardy (2010) Stability of the triangular Lagrange points beyond Gascheau’s value, Celest. Mech. Dyn. Astron. 107, 145–155 (Gascheau 1843 precedes Routh) (opens in a new tab)
Source Lagrange, J.-L. (1772). Essai sur le problème des trois corps. Prix de l’Académie Royale des Sciences de Paris, tome IX.