DWG NO OD-2026-003
TITLE

GD&T in Zero Gravity

ISSUE
REV C
DATE 2026-08-02
SCALE NTS

On a workbench, gravity is a silent inspector. Parts sit flat, brackets hang true, and a slightly warped panel announces itself by rocking on the surface plate. In orbit, none of that exists. The only thing holding your geometry together is the drawing — which is why geometric dimensioning and tolerancing stops being paperwork and becomes the mission.

A position callout of ⌖ Ø0.05 A B C looks like bureaucratic fine print until you picture a star tracker bolted to a panel that was machined in a 1-g shop, shipped through 8 g of vibration, and is now floating in vacuum at a 90-degree thermal swing. The feature control frame is the only sentence in the entire assembly that survives all three environments unchanged.

The Datum Is the Spacecraft

Every GD&T scheme begins with a datum reference frame, and spacecraft are unusually honest about theirs. Datum A is almost always the primary structural deck — the interface plate that everything else bolts to. B and C are typically machined edge or a pair of tooling holes that were reamed before the first bracket was ever modeled.

A Ø0.05 A B 4× Ø12 THRU · POSITION PER FCF FCF SURVIVES: 1-G SHOP → 8-G VIBE → VACUUM
FIG 1.1 — BRACKET PLATE, POSITION CALLOUT SCALE 1:1

Three Habits That Survive Orbit

Gravity is the cheapest fixture ever made. Orbit charges interest on every assumption it let you skip.

The practical takeaway for modelers: build your CAD assemblies the way the drawing will be inspected. Mate to datum planes that correspond to real surfaces, suppress nothing that inspection would measure, and let the feature control frame — not the mate folder — be the source of truth.

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