Development of configuration design of payload to meet its functional requirement.
Coordination with spacecraft design team to incorporate spacecraft thermal and structural requirements in payload configuration as well as its structural and thermal design.
Structural and thermal design of Payload subsystems and complete payload. (Through Identified outsourcing team)
Formulating test philosophy for testing and qualification of Payload subsystems and complete payload.
Identification of Vendors for fabrication of payload mechanical hardware and coordination with vendors for hardware fabrication and realization.
Coordination with various agencies for identification of test facilities to carry out required tests on subsystem and integrated payload based on finalized test philosophy.
Payload integration and thermal implementation.
Payload Safety and Transportation.
Requirements
3-5 years of experience in design
Hands-on experience of working on simulation tools such as FEM and FDM.
Good understanding of process planning.
Good understanding of Mechanical Drawings, Manufacturing Processes, Heat Treatment, and surface treatment.
Good understanding of Structural (Especially vibration) and Thermal Design.
Education - UG: Any Graduate, PG: Any Postgraduate