Antenna general arrangements, interface drawings and weight statements are included in this document for use during the remainder of the MPTS studies. Detail thermal and structural evaluations have been performed to determine the limitations the structure impose on electronic layout and phase front control concepts. Mechanical options to a fully electronic control system have been identified and are shown to desensitize the tolerance on structural assembly accuracy and impact of thermal deflections over a wide range of sun-to-spacecraft geometries.
RkJQdWJsaXNoZXIy MTU5NjU0Mg==