Lead hardware systems for drone platforms, ensuring reliability and performance in demanding environments.
Posted by employer 13 hours ago
First seen on Joblaze 6 hours ago
Last verified on the company career page 6 hours ago
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Not disclosed in this posting: compensation, visa sponsorship.
Joblaze summary
The Hardware Systems Lead for Applied Intuition's drone program is responsible for the hands-on engineering of hardware that ensures the reliability and performance of drones in flight. This role requires expertise in mechanical and electrical systems, with a focus on survivability and integration of various sensors and components. Ideal candidates will have over a decade of experience in hardware engineering for aircraft, demonstrating a strong grasp of systems-level design and testing. The position is situated within a rapidly growing company that emphasizes collaboration across multiple engineering disciplines.
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From the original posting
ABOUT THE ROLE
As Hardware Systems Lead for our drone program, you will be the hands-on chief engineer for the hardware that carries our autonomy into the air. You will understand the full system, mechanical and electrical, and own the question that matters most in flight: will it survive, and will it keep working when the aircraft is hundreds of feet up? You will architect, build, test, and break hardware, then use what you learn to make it lighter, tougher, and more reliable. Your decisions will define how Applied's hardware performs in flight, in wind, vibration, shock, temperature swings, and moisture, and you will work closely with autonomy, software, and flight test teams to get aircraft flying.
At Applied Intuition, you will:
Own the end-to-end hardware architecture, mechanical and electrical, for Applied Intuition’s drone platforms
Be hands-on: prototype, build, integrate, debug, and test hardware on real aircraft, not just review designs
Define and drive survivability: determine how sensors, compute, avionics, harnesses, connectors, and enclosures will hold up to vibration, shock, hard landings, thermal extremes, dust, water ingress, and EMI
Lead integration of sensors (cameras, lidar, radar, GNSS/IMU), compute, power systems, communications, and flight controllers onto airframes
Own size, weight, and power (SWaP) tradeoffs, balancing performance, flight time, payload capacity, and cost
Define hardware requirements and reference architectures that scale across aircraft configurations
Plan and run environmental, durability, and flight testing, analyze failures and crashes, and drive root cause and design fixes
Be the technical authority and escalation point for hardware tradeoffs across mechanical, electrical, avionics, software, autonomy, and flight test
Lead hardware design reviews, set engineering standards, and mentor other engineers
Support flight test campaigns, demonstrations, and field operations
We’re looking for someone who:
BS/MS in Aerospace, Mechanical, Electrical, Mechatronics, or a related field
10+ years of hands-on hardware engineering experience on drones, UAS, or other aircraft
Strong command of the whole hardware system: airframe and structures, electrical architecture, power distribution, harness design, avionics, and how they interact
A track record of designing hardware to survive demanding environments, with real experience in vibration, shock, ingress protection, thermal management, and EMI/EMC
Hands-on experience in the lab and in the field: building prototypes, wiring and debugging systems, running flight tests, and diagnosing failures and crashes
Experience integrating sensors such as cameras, lidar, radar, and GNSS/IMU, along with compute and flight control hardware, onto airborne platforms
Experience with SWaP optimization and lightweight design, including composites and carbon fiber
Experience with reliability and qualification testing (environmental testing, HALT, flight-hour tracking)
Systems-level thinking and the ability to make architecture decisions and defend them
Experience designing for manufacturability and field serviceability
Nice to have:
Experience with fixed-wing, multirotor, or VTOL platforms
Familiarity with aerospace standards such as DO-160 or MIL-STD-810 and MIL-STD-461
Experience with propulsion, battery, or power system integration
Standard company text repeated across Applied Intuition's postings is omitted here.