Planetary Mass Estimation Notes
1) Overview of planetary mass estimation
Planetary mass controls orbital motion, surface gravity, and the ability to retain an atmosphere. This calculator estimates mass using four classical routes: surface gravity with radius, escape velocity with radius, bulk density with radius, or orbital period with semi-major axis. Outputs are shown in kilograms plus Earth and Jupiter mass units for comparison.
2) Surface gravity with radius
With surface gravity g and mean radius R, use g = GM/R², so M = gR²/G. Using Earth values (g ≈ 9.80665 m/s², R ≈ 6371 km) returns M ≈ 5.97×10²⁴ kg, essentially 1 M⊕. This method fits lander and atmospheric constraints.
3) Escape velocity with radius
Escape velocity links to the gravitational potential: vesc = √(2GM/R). Rearranged, M = vesc2R/(2G). For Jupiter, vesc ≈ 59.5 km/s and R ≈ 71492 km gives ≈ 1.90×10²⁷ kg (about 317.8 M⊕) after rounding.
4) Density with radius
If bulk density ρ is known, compute volume and multiply: M = ρ(4/3)πR³. Rocky worlds commonly fall around 3–5.5 g/cm³, while gas giants are often near 1–2 g/cm³. Because mass scales with R³, accurate radius is crucial.
5) Kepler orbit for system mass
Kepler’s third law gives total system mass from orbit size and period: Mtotal = 4π²a3/(GT2). With a = 1 AU and T = 365.256 days, the result is near the Sun’s mass (≈ 1.99×10³⁰ kg, or ≈ 332,946 M⊕). This is best for stars, planets with moons, and exoplanet hosts.
6) Units and reference scaling
Inputs are converted to SI internally (km→m, days→s, g/cm³→kg/m³, AU→m). Results are reported in kg plus M⊕ and MJ. Always match the unit selectors to your numbers to avoid order-of-magnitude mistakes.
7) Assumptions and uncertainty
The relations assume a near-spherical body and a representative mean radius. Oblateness, rotation, and layered structure can shift effective surface gravity and escape speed. In practice, measurement uncertainty and rounding of constants dominate, so small percent-level differences from published values are normal.
8) Practical applications
Mass supports mission design (injection, landing, ascent), planetary classification, and habitability screening. Combined with radius, mass yields mean density for composition estimates. With mass and temperature, you can assess atmospheric escape and volatile retention. When possible, compute mass using two methods as a consistency check.