Lead Rocket Test Engineer - Vibration & Hot-Fire Lab

RocketForce Technologies LLC

Redmond (WA)

On-site

USD 77,000 - 142,000

Full time

41 hours ago
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Job summary

L3Harris is seeking a Senior Associate, Integration/Test Engineering for our Redmond, WA facility. The role involves coordinating vibration, hot-fire, and component-level testing of rockets, supporting monopropellant, bipropellant, and electric thrusters for in-space applications.

Responsibilities include designing test methods, configuring data acquisition, organizing technician tasks, and analyzing test data.

Qualifications

  • Bachelor’s degree required; 2+ years Integration/Test experience.
  • Graduate degree or equivalent with 0–2 years of Integration/Test experience.
  • In lieu of a degree, 6+ years Integration/Test experience.

Responsibilities

  • Develop, design, and evaluate test methods, procedures, and equipment used in testing systems and components.
  • Conduct rocket engine vibration and hot firing tests in a vacuum chamber with proper data acquisition and control.
  • Monitor and maintain data acquisition, control, and mechanical systems in the vibration lab.
  • Organize technician work force tasks to accomplish test objectives.
  • Assist in planning test setup requirements through reviews, meetings, and proposals.
  • Analyze engine and facility test data for monitoring hardware and equipment.
  • Participate in the Emergency Response Team.
  • Possess the ability to obtain a US Secret Clearance.
  • Possess the ability to obtain respirator certification.

Skills

Leadership
Communication
Teamwork

Education

Bachelor's degree in aerospace / mechanical / chemical engineering
Graduate degree or equivalent with 0–2 years of Integration/Test experience
In lieu of a degree, minimum of 6 years of Integration/Test experience

Job description

L3Harris is seeking a Senior Associate, Integration/Test Engineering for our Redmond, WA facility. The role involves coordinating vibration, hot-fire, and component-level testing of rockets, supporting monopropellant, bipropellant, and electric thrusters for in-space applications.

Responsibilities include designing test methods, configuring data acquisition, organizing technician tasks, and analyzing test data.

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