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Design and develop spacecraft electronics ranging from PCBAs to full systems, including power, digital, and mixed-signal designs. Responsibilities include component selection, circuit board design, board bring-up, debugging, environmental qualification testing, spacecraft integration, test equipment development, and test-script creation. The intern will collaborate with engineers, technicians, managers, and external stakeholders during a three-month internship.

Support analysis, design, testing, measurement, and qualification of RF and microwave hardware for spacecraft. Operate antenna measurement systems, conduct environmental testing, perform development and production tests, and collaborate with engineers, technicians, managers, customers, and other stakeholders to integrate RF work into satellite systems.

Develop spacecraft guidance, navigation, and control algorithms for attitude and orbit control. Build high-fidelity models and simulations of spacecraft dynamics, actuators, and sensors; test algorithms through unit testing, integrated simulation, and hardware-in-the-loop environments; support flight software verification, spacecraft operations, vehicle architecture, and actuator and sensor trades.

Supports aerospace dynamics engineering for satellite ground transportation, launch, deployment, and on-orbit operations. Responsibilities include dynamic analysis, testing, correlation, hand calculations, computational methods, development testing, and cross-functional hardware trades. The intern will own a mentored project, apply engineering knowledge to spacecraft hardware, and collaborate with technicians, engineers, and managers. This is a 12-week, in-person internship at K2 Space headquarters in Torrance.

Three-month, in-person Mechanical Engineering Internship developing complex spacecraft structures and mechanisms. Responsibilities include designing, analyzing, testing, and building mechanical systems; performing hand calculations and computational analyses; conducting development tests; supporting hardware trade studies; and owning a mission-impacting project with mentorship. Candidates must be enrolled in an engineering degree program and have at least six months of technical engineering experience outside the classroom. CAD experience and mechanical hardware project experience are preferred.

Manage advanced payload integration across the spacecraft lifecycle, from proposals and design through testing, launch, and on-orbit commissioning. Serve as the primary customer and partner interface, define and negotiate mechanical, electrical, software, power, and mission interfaces, and lead verification, validation, and sell-off activities. Coordinate vehicle engineering, avionics, software, propulsion, thermal, and integration teams while improving payload engineering processes and mentoring team members.

Design, analyze, build, align, test, and qualify precision optomechanical assemblies for satellite optical payloads. Responsibilities include lens and mirror mounting, optical alignment and stability budgets, structural and thermal analysis, vibration and thermal-vacuum testing, design reviews, hardware iteration, and production support. The role collaborates across optical, thermal, structures, GNC, metrology, and manufacturing teams to deliver flight-qualified hardware for space missions.

Own compensation and equity strategy, including benchmarking, pay frameworks, offer reviews, merit and promotion recommendations, Carta equity administration, and equity modeling. Build workforce dashboards and analytics for leadership, maintain HR data integrity, and support workforce planning. Lead responsible AI tool adoption across People Operations and provide compensation and workforce analyses for executives, board materials, and investors.

Own spacecraft and constellation hardware reliability strategies, requirements, models, allocations, and testing programs. Lead HALT/HASS, accelerated life testing, reliability growth, statistical modeling, root-cause investigations, FRACAS, and corrective actions. Integrate test and flight telemetry data into reliability predictions, flow down requirements, advise leadership on risk trade-offs, and mentor reliability engineers. Partner with design, systems, test, and manufacturing teams to improve robustness and support high-volume satellite production.

Leads spacecraft dynamics analysis and testing across transportation, launch, deployment, and on-orbit environments. Develops finite element, time- and frequency-domain models, simulation software, coupled loads analyses, vibroacoustic models, jitter and pointing analyses, and modal test methodologies. Owns qualification and acceptance testing, model correlation, loads and environment derivation, technical documentation, and shared analysis tooling. Provides technical direction, mentors engineers, and delivers data-driven guidance for reliable, mass-producible spacecraft.