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6 дней назад

Senior Combustion Devices Engineer II / Principal Combustion Devices Engineer (Rocket Propulsion)

132 000 - 270 000$
Формат работы
onsite
Тип работы
fulltime
Грейд
senior
Английский
b2
Страна
US
Вакансия из списка Hirify.GlobalВакансия из Hirify Global, списка международных tech-компаний
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Описание вакансии

Текст:
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TL;DR
Senior Combustion Devices Engineer II / Principal Combustion Devices Engineer (Rocket Propulsion): Developing combustion devices for the 200,000 lbf Archimedes rocket engine, including preburners, main injectors, thrust chamber assemblies, and vacuum nozzles, with an accent on design analysis, qualification, manufacturing, and flight support. Focus on designing reusable propulsion hardware, interpreting test data, integrating with turbomachinery and engine systems, and enabling high-cadence tests, flights, and re-flights.

Location: Long Beach, California, United States; onsite at hirify.global's headquarters. Candidates seeking to work in U.S. offices must meet applicable ITAR eligibility requirements, such as being a U.S. citizen, lawful permanent resident, refugee, asylee, or eligible to obtain the required authorization.

Base salary: $132,000–$270,000 USD annually. Total compensation including equity: $164,500–$319,725 USD annually.

Company

hirify.global is an end-to-end aerospace company developing rockets, spacecraft, and critical spaceflight subsystems, including the reusable Neutron launch vehicle.

What you will do

  • Design combustion devices such as preburners, main injectors, thrust chamber assemblies, and vacuum nozzles for the Archimedes engine.
  • Perform design analysis and trade studies to meet program targets.
  • Define component requirements, test plans, and flight qualification plans.
  • Collaborate with turbomachinery, engine systems, manufacturing, and build engineering teams.
  • Support testing and launch operations by interpreting data and developing solutions for high-cadence tests, flights, and re-flights.
  • Design cost-effective, manufacturable components for an iterative reusable rocket program.

Requirements

  • Bachelor's degree in engineering or equivalent experience.
  • For Senior level: 8+ years of combustion device design experience.
  • For Principal level: 12+ years of combustion device design experience.
  • In-depth knowledge of combustion and fluid dynamics, heat transfer, and structural mechanics.
  • Fundamental understanding of design principles and manufacturing methods.
  • U.S. office roles require eligibility under applicable ITAR and U.S. government export regulations.

Nice to have

  • Master's degree or PhD.
  • Advanced proficiency in NX, ANSYS Mechanical, StarCCM, MATLAB, or GD&T.
  • Experience with TDK, ROCCID, PERCORP, CEA, or ROCETS.
  • Reacting-flow CFD and high-speed data or video analysis experience.
  • Experience designing reusable, propulsively landing rocket engines.
  • Experience in an iterative and scrappy development environment.

Culture & Benefits

  • Paid vacation and sick time, 11 paid holidays, and paid parental leave.
  • Medical, dental, vision, disability, life insurance, flexible spending, and dependent care benefits.
  • 401(k) retirement plan with company match and an employee stock purchase program with a 15% discount.
  • Company equity as part of total compensation.
  • Additional benefits include subsidized EV charging, onsite fitness centers where available, gym discounts, snacks, beverages, and employee discounts.
  • The role may involve prolonged sitting, standing, walking, computer work, and occasional exposure to moderate noise, dust, and fumes in production areas.

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