Lead Integrated Functional Capability (IFC) for NATO Business Area, managing interface control, integration, and certification across systems engineering disciplines.
Lead Integrated Functional Capability (IFC) for NATO Business Area, managing interface control, integration, and certification across systems.
Locations (2)
Rancho Bernardo, California, United States
San Diego, California, United States
Responsibilities
Serve as technical authority for IFC on the program
Define and execute IFC certification process for software and hardware builds
Lead and/or chair IFC-related meetings
Evaluate Engineering Change Proposals and change requests
Develop strategic IFC roadmap
Requirements
Bachelor’s of Science in a STEM discipline (e.g., Systems Engineering, Electrical Engineering, Computer Engineering, Computer Science, Aerospace Engineering)
Master’s degree with 7+ years
PhD with 4+ years
Nice to have: Prior experience as an IFC Lead, Integration Lead, or senior SE
Nice to have: Experience with IFC certification processes
The SE&I Engineer will serve as a technical contributor and integrator for next generation life support systems to lunar lander vehicles, evaluating system designs, documentation, and analyses to ensure compliance with interface, performance, and safety requirements for Artemis missions.
Responsibilities
Perform systems engineering and integration (SE&I) assessments of Life Support System to lunar lander vehicles and related subsystem documentation, analyses, and requirements.
Review & develop ICDs, (other e.g. ConOps, IRD, DRDs, IDDs, GR&As, V&V evidence) modeling outputs, and system specifications for completeness and technical adequacy.
Assess partner-provided designs for compatibility with crew interfaces and vehicle or habitat systems
Coordinate with NASA program personnel, suit vendor teams, and vehicle contractors to clarify requirements, communicate findings, and support integrated system development.
Support resolution of complex system level issues through analysis, trade studies, and technical review.
Requirements
Bachelor's degree in engineering (mechanical, aerospace, systems, or related discipline)
Nice to have: Spacesuits & PLSS design
Nice to have: integration
Nice to have: testing
Nice to have: human spaceflight development programs
Technical contributor and integrator for next generation life support systems to lunar lander vehicles.
Responsibilities
Perform systems engineering and integration assessments of Life Support System to lunar lander vehicles and related subsystem documentation, analyses, and requirements.
Review & develop ICDs, ConOps, IRDs, DRDs, IDDs, GR&As, V&V evidence, modeling outputs, and system specifications for completeness and technical adequacy.
Assess partner-provided designs for compatibility with crew interfaces and vehicle or habitat systems.
Coordinate with NASA program personnel, suit vendor teams, and vehicle contractors to clarify requirements, communicate findings, and support integrated system development.
Support resolution of complex system level issues through analysis, trade studies, and technical review.
Requirements
Bachelor's degree in engineering (mechanical, aerospace, systems, or related discipline)
Nice to have: Spacesuits & PLSS design
Nice to have: integration
Nice to have: testing
Nice to have: human spaceflight development programs
Lead systems engineering for a next-generation autonomous Group 5 Rotorcraft, owning architecture, requirements, verification, and cross-team interfaces.
Compensation
The salary range for this role is an estimate based on a wide range of compensation factors, inclusive of base salary only. Actual salary offer may vary based on (but not limited to) work experience, education and/or training, critical skills, and/or business considerations. Highly competitive equity grants are included in the majority of full time offers; and are considered part of Anduril's total compensation package.
Responsibilities
Own system end-to-end definition and architecture
Enforce configuration control and risk management
Assist in test planning and validation
Lead milestone and gate reviews
Deploy Agile Systems Engineering governance
Requirements
Bachelor's degree in Systems Engineering, Aerospace Engineering, Mechanical Engineering, Electrical Engineering, or equivalent
Nice to have: Hybrid/electric powertrains
Nice to have: Model-based Product Line Engineering (MBPLE)
Seeking a highly motivated Chief Engineer - Space to support the mission-oriented efforts of developing and bringing to market Radioisotope Power Systems (RPS) technologies. Leadership of technical and engineering aspects within space system design, development, deployment lifecycle, and production.
Compensation
The anticipated salary band for this position is $195,000 - $245,000.
Responsibilities
Act as Design Authority for space scope area
Provide technical leadership on Zeno space projects
Define and interpret high level engineering requirements to support Product, Program, and/or Customer needs
Support technical project meetings for space initiatives by providing real-time technical guidance, operational support, and informed decision-making
Generate, review, and/or approve technical work products for design applicability, adequacy, and accuracy
Support the development and deployment of nationally important solutions through mission engineering, MBSE, and systems architecture.
Compensation
$77,600 - $97,000 - $116,400 Annual
Responsibilities
Apply Mission Engineering, Traditional Systems Engineering (TSE) and Model-Based Systems Engineering (MBSE) in support of our sponsor’s mission objectives and outcomes
Translate mission needs, operational constraints, and capability gaps into system concepts, designs, and technical solutions
Develop and refine system architectures, requirements, interfaces, data flows, and integration dependencies
Support integration, testing, verification, validation, deployment planning, and technical transition
Collaborate with multidisciplinary teams on technical deliverables, documentation, and presentations
Lead the organization responsible for translating customer and business needs into safe, certifiable, and supportable aircraft systems.
Responsibilities
Lead and develop a multidisciplinary systems engineering team
Build a high-performing engineering culture through coaching, mentoring, succession planning, workforce planning, performance management, and employee engagement
Own systems engineering execution for new product development, product enhancements, certification programs, and sustaining engineering across the full lifecycle
Provide technical oversight of system architectures, requirements decomposition, interface definitions, trade studies, design reviews, integration, verification, validation, and certification evidence
Ensure effective application of SAE ARP4754A and ARP4761A principles
Requirements
Bachelor's degree in Systems, Electrical, Computer, Software, Mechanical, Aerospace, or a related engineering discipline
The likely salary range for this position is $178,500 - $241,500.
Responsibilities
Maintain the integrated architecture baseline, interface catalog, dependency map, assumptions/constraints register, and architecture action log.
Translate Chief Architect direction into coordinated domain work packages, interface-control documents, integration sequencing, and acceptance criteria.
Lead cross-domain design workshops, technical interchange meetings, integration engineering reviews, and production-readiness preparation.
Verify traceability from approved requirements through architecture, detailed design, build configuration, test evidence, operational documentation, and deployment decision.
Identify interface conflicts, circular dependencies, boundary ambiguities, and sequencing risks; drive owners to closure before they become production issues.
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