Attitude Control Motor

E2171972 UNEXPLORED

The Attitude Control Motor is a solid-fueled rocket motor used to steer and stabilize a spacecraft’s launch abort system during emergency escape maneuvers.

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All labels observed (1)

Label	Occurrences
Attitude Control Motor canonical	1

Referenced by (1)

Full triples — surface form annotated when it differs from this entity's canonical label.

Pad Abort 1 → usedComponent → Attitude Control Motor ⓘ

subject linked to: Pad Abort 1 test