Serves as primary responsible engineer for all technical and regulatory contract deliverables through execution of an LSA from contract effective date to include mission integration, dynamics model, mass properties, mechanical & electrical interface specifications, launch vehicle separation configuration & analysis, Range Safety, FAA/FCC licensing, hazardous procedures, launch site campaign planning and integration and test procedure definition. The role is responsible for launch vehicle and recovery requirements definition for Varda Space Vehicles, delivery of all technical and regulatory contract deliverables to the launch provider per the Launch Services Agreement (LSA), definition of launch vehicle ICD with the launch provider, and management and execution of launch site I&T and capsule recovery procedures.