Antenna Systems Integration Engineer
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About the role
What you will do:
Own assembly-level coordination between structural, RF, and deployment subsystem teams, tracking interface compliance.
Maintain and drive resolution of IAS interface control documents (ICDs), ensuring parameter handoffs between teams are defined, current, and verified.
Serve as the primary on-site technical representative for the IAS Lead Engineer (remote) during integration activities, test campaigns, and anomaly resolution.
Track assembly-level requirements through to hardware verification artifacts using requirements management and V&V closure tools (DOORS, Jama, or equivalent); flag gaps before they become schedule drivers.
Support and coordinate antenna deployment and structural test campaigns, including pre-test review, test execution support, and post-test data review.
Develop and maintain integration procedures, assembly checklists, and interface verification records.
Identify and escalate integration risks early: incomplete interface definitions, undocumented design changes, test article discrepancies.
Required qualifications:
BS or MS or Ph.D. in Aerospace, Mechanical, or Systems Engineering, or equivalent.
Experience with hardware integration on spacecraft or flight structures programs. AIT, structures integration, or systems engineering experience with hands-on hardware responsibility.
2-3 years of hands-on experience with deployable structures, gossamer systems, or large space mechanisms. Directly relevant domain experience is required, not just general spacecraft structures.
Demonstrated ability to read and maintain ICDs, interface matrices, and assembly-level requirements.
Experience working across subsystem teams to resolve interface discrepancies.
Strong written and verbal communication; this role is the translation layer between multiple teams.
Preferred qualifications:
Familiarity with PLM/configuration management tools (Windchill, Teamcenter, Arena, or equivalent) and requirements management tools (DOORS, Jama, or equivalent).
Experience running or coordinating test campaigns for flight hardware.
Exposure to model-test correlation or V&V planning for structural systems.
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