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Spacecraft Bus Structure

Assembly

Three-axis-stabilized box structure with an Earth-facing instrument bench whose thermal distortion is controlled to keep instrument pointing within microradians. A full specification article for this item is being written. Meanwhile its bill of materials and connections are below.

Bill of materials for Spacecraft Bus Structure

4 top-level lines as of r188076
# Item / sub-assembly Part no. Qty/assy Ext. qty Parts Type
1 Instrument Optical Bench weather-satellite-optical-bench 1× 1 · part
2 Sheet Metal Panel sheet-panel 6× 6 · part
3 Fastener Set fastener-set 5× 5 · part
4 Wire Bundle wire-bundle 3× 3 · part