GNC Engineer II - Mission Design

at  Rocket Lab USA

ABOUT ROCKET LAB

Rocket Lab is a global leader in launch and space systems. The rockets and satellites we build and launch enable some of the most ambitious and vital space missions globally, supporting scientific exploration, Earth observation and missions to combat climate change, national security, and exciting new technology demonstrations. Our Electron rocket has provided reliable access to orbit since 2018, becoming one of the most frequently launched rockets in the world. Neutron will be our next rocket on the launch pad, an advanced 13-tonne payload class, reusable rocket to launch the mega constellations of the future. Our space systems business includes our extensive line of satellites and components that have enabled more than 1,700 missions including the James Webb Space Telescope, NASA Psyche Mission, Artemis I, Mars Ingenuity helicopter, and more.
Join our pioneering team and launch your career to new heights!

YOU’LL BRING THESE QUALIFICATIONS:

• 1+ years of relevant experience
• Master’s degree or higher in Aerospace Mechatronics or equivalent qualification (Bachelor’s degree can be considered for Engineer I level)
• A thorough fundamental understanding of 3DOF rocket dynamics
• A thorough fundamental understanding of orbital mechanics
• Experience with optimization for launch-vehicle or spacecraft missions

THESE QUALIFICATIONS WOULD BE NICE TO HAVE:

• 3+ years of experience
• Experience with GMAT or STK
• Experience with software development in Python or MATLAB
• Experience in development/implementation of a basic 3DOF propagator for LEO, lunar, or interplanetary trajectory from fundamental equations of motion
  If the above sounds like you, apply now!

WHAT YOU’LL GET TO DO:

Based out of Rocket Lab’s Auckland, NZ office, the GNC Engineer – Mission Design is responsible for general mission design including trajectory design and optimization, auto-sequence planning & design, Monte Carlo analysis, configuration management, and any other mission design, launch operations, verification and validation tasks as required.

KEY RESPONSIBILITIES:

• Assisting with trajectory optimization/design for launch vehicle orbital missions.
• Assisting with auto sequence design (maneuvers, telemetry, ground station contacts), implementation and verification for orbital flight, stack tests and wet dress rehearsals
• Analysis and missionisation of optimised 3DOF trajectories for implementation in 6DOF and flight scenarios
• Monte-Carlo analysis pre-flight, launch day and post-flight analysis
• Design and verification of spacecraft separation sequences and dynamics
• Assisting with all areas of GNC development and maintenance for Electron, Neutron and/or other programmes including
• Core GNC R&D (Guidance, Navigation, and Control)
• Vehicle parameter modelling / prediction and/or configuration control
• 6DOF simulator design and development
• Launch and HITL operations