Glidepath Rate of Descent

The rate of descent that holds a glidepath, from the ground speed: ROD = ground speed x 101.27 x tan(angle) ft/min, and the path itself is 6076.12 x tan(angle) ft/nm -- 318 ft/nm at a standard 3.00 degree ILS, the exact FAA TERPS figure that fixes the tangent form. At 120 kt on a 3-degree path that is 637 ft/min, which the 'ground speed x 5' rule rounds to 600. Because it scales with GROUND speed, a tailwind or a faster approach demands a higher descent rate to stay on the same path. A planning aid, not a clearance; the approach chart and the pilot in command govern.

Run the calculator

Formula and source

rod_fpm = ground_speed_kt x 101.269 x tan(glidepath_angle); ft_per_nm = 6076.12 x tan(glidepath_angle). The 101.269 converts knots (nm/hr) to ft/min (x 6076.12 / 60).

Required rate of descent on a glidepath (FAA Instrument Flying Handbook; TERPS Order 8260.3), by name; the approach chart and the pilot in command govern.

Audience

This tile is built for mechanics and the adjacent professions in the Mechanic - Auto, Marine, Aviation group. The interactive calculator runs entirely in your browser. No account, no fee, no advertising, no tracking.

Related tools

Posture

Rough Logic answers the math question the working professional asks on the job. The site is a calm, fast, ad-free, account-free, ever-free reference. It does not interpret code. It does not replace the licensed professional. It does not store your inputs. The Authority Having Jurisdiction governs all installations and inspections.