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Gravity & Orbits

Orbital mechanics, solar system, tidal forces, and N-body simulations

27 simulators
NewUniversity / research

Schwarzschild Orbit Precession (Rosette)

Schwarzschild geodesic in the φ-form d²u/dφ² + u = 1/L² + 3u² (G = c = M = 1) integrated by RK4. The closed Newtonian ellipse is replaced by an orange precessing rosette with apsidal advance Δφ ≈ 6πM/[a(1 − e²)] per orbit — the same mechanism that produces the historic 43″/century perihelion shift of Mercury. Horizon r = 2M and ISCO r = 6M annotated.

Launch Simulator
NewUniversity / research

ISCO & Photon Sphere (V_eff)

Schwarzschild effective potential V_eff(r) for massive (timelike) and photon (null) test particles in geometric units. Sliding angular momentum L collapses the stable / unstable circular pair into the innermost stable circular orbit r_ISCO = 6M (the inner edge of accretion discs); for photons the unstable photon sphere r = 3M defines the inner ring of black-hole shadow images.

Launch Simulator
NewUniversity / research

Einstein Ring & Paczyński Microlensing

Point-mass thin lens (weak-field GR): lens equation β = θ − θ_E²/θ gives two images θ_± = ½(β ± √(β² + 4θ_E²)) with magnifications μ_± = ½[(u² + 2)/(u√(u² + 4)) ± 1], u = β/θ_E. Animated source transit at impact parameter u₀ over timescale t_E renders the canonical symmetric Paczyński light curve and the full Einstein ring θ_E = √(4GM·D_LS/(c² D_L D_S)) at perfect alignment.

Launch Simulator
NewUniversity / research

Gravitational Wave Binary Chirp (Inspiral)

Leading-order post-Newtonian inspiral of a compact binary: f(τ) ∝ τ^(−3/8), strain h(t) ∝ M_c^(5/3) f^(2/3) / D_L. Tune component masses m₁, m₂ and luminosity distance D_L; live h(t) and f(t) traces with the orbiting bodies on the side. The chirp mass M_c = (m₁m₂)^(3/5)/(m₁+m₂)^(1/5) is the very quantity LIGO/Virgo measures from the early inspiral; the frequency freezes at the Schwarzschild ISCO.

Launch Simulator
NewUniversity / research

Shapiro Time Delay (4th GR Test)

A radio signal grazing the Sun picks up an excess one-way travel time Δt ≈ (2GM/c³) ln[(r_E + r_E cos α)(r_R + r_R cos β)/b²] on top of the Newtonian light-time. Cassini, Mariner and Viking presets, with the round-trip delay readout in microseconds and an animated bent-photon path against a straight Newtonian baseline. The Cassini 2003 conjunction constrains |γ_PPN − 1| < 2 × 10⁻⁵ — the strongest weak-field GR test to date.

Launch Simulator
NewUniversity / research

Three-Body Figure-Eight

Equal masses: Chenciner–Montgomery choreography in 2D (RK4, periodic orbit).

Launch Simulator
NewUniversity / research

Restricted 3-Body (map)

CRTBP: escape vs collision vs chaos proxy; μ slider.

Launch Simulator
NewSchool

Multistage Rocket (Tsiolkovsky)

Δv per stage; sum vs single-stage with same total propellant.

Launch Simulator
NewSchool

Orbital Debris & Kessler (toy)

LEO shell: n = N/V, collision rate ∝ N²; optional fragment cascade.

Launch Simulator
NewSchool

Gravity-Assist Fly-By

Planet frame |u_out|=|u_in| rotated by δ; star frame v = V + u — Δ|v| from moving planet.

Launch Simulator
FeaturedSchool

Orbit Simulator

Launch satellites. Achieve circular, elliptical orbits, or escape.

Launch Simulator
School

Solar System

Interactive scaled model with time controls and orbital data.

Launch Simulator
FeaturedSchool

Gravity Sandbox

Place masses and watch N-body gravitational interactions unfold.

Launch Simulator
School

Kepler's Laws

Elliptical orbits with equal-area sweeps visualized.

Launch Simulator
School

Escape Velocity

Launch from different planets and see trajectory results.

Launch Simulator
NewUniversity / research

Gravitational Lensing

Massive objects bending light. Visual distortion effects.

Launch Simulator
NewUniversity / research

Lagrange Points L1–L5

CRTBP effective potential; L1–L5; Coriolis test particle.

Launch Simulator
NewSchool

Earth–Moon Tides

Equilibrium tide bulges; orbit speed; ~12.4 h spacing note.

Launch Simulator
NewSchool

Binary Star (circular)

COM orbits; r₁,r₂; Kepler T² ∝ a³/(M₁+M₂).

Launch Simulator
NewUniversity / research

Roche Limit

Fluid d ≈ 2.456 R_p (ρ_p/ρ_s)^(1/3); vs orbit distance.

Launch Simulator
NewSchool

Space Elevator Tether

1D tension vs height; peak near GEO (normalized model).

Launch Simulator
NewSchool

Hohmann Transfer

Coplanar circles r₁,r₂; transfer ellipse; Δv₁, Δv₂ from vis-viva.

Launch Simulator
NewSchool

Geostationary Orbit

ω²r = GM/r² from sidereal vs solar day; Earth-fixed view with sub-satellite longitude.

Launch Simulator
NewSchool

Orbital Decay (Atmosphere)

Toy perigee drag: shrinking, circularizing ellipse; ISS lifetime intuition.

Launch Simulator
NewUniversity / research

Mercury Perihelion Precession

GR Δω per orbit vs Newton; ~43″/century readout; amplified animation.

Launch Simulator
NewSchool

Earth–Moon Barycenter Wobble

Heliocentric path of Earth’s center: barycentric ellipse plus lunar epicycle (exaggerated).

Launch Simulator
NewUniversity / research

Oberth Effect

Same prograde Δv at peri vs apo on one ellipse; higher ε when burning deep.

Launch Simulator