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Technical diagram showing the exploded view of the MultiMission Modular Spacecraft (MMS) components used for Landsat-D. The illustration displays labeled subsystems including the shuttle cradle load pin at the top, transition adapter (instrument module interface), attitude control system, power system, signal conditioning and control unit, module support structure, L/V umbilical connector, communication and data handling system, Delta interface, and propulsion module at the bottom. All components are shown separated to illustrate their individual structure and how they integrate together.

MultiMission Modular Spacecraft – Landsat-D

Exploded view diagram of the MMS platform showing the modular subsystems and components that form the standardized spacecraft bus for the Landsat-D Earth observation mission.

Image Credit: NASA
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Image CreditNASA
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