Spacecraft Bus Design and Integration

The contract involves the design, development, and integration of the GLIMR spacecraft bus, focusing on key subsystems such as structural, thermal, power, and attitude control. The goal is to ensure seamless compatibility of the spacecraft bus with the designated payload and launch vehicle, highlighting a comprehensive approach to spacecraft system engineering. Issued by the NASA Langley Research Center, this subcontract falls under the industrial classification for aircraft and aerospace product manufacturing. The work is to be performed in Hampton, aligning with NASA's strategic objectives in space exploration and technology advancement. This project emphasizes the integration of multiple technical domains to deliver a fully functional and reliable spacecraft bus for the GLIMR mission.