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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.

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