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Propulsion Engineer II, Engine Systems (pipeline)
Исключительная возможность работать над амбициозным проектом Neutron в одной из ведущих космических компаний мира. Высокий балл за инновационность и реальный вклад в будущее космонавтики.
Сложность вакансии
Высокая сложность обусловлена строгими требованиями ITAR, необходимостью глубоких знаний в криогенных системах и термодинамике, а также ответственностью за разработку критически важных узлов двигателя.
Анализ зарплаты
Предлагаемая позиция соответствует уровню Middle (Engineer II) в аэрокосмической отрасли США. Рыночные оценки для инженеров по двигательным установкам в Миссисипи и аналогичных центрах (Stennis) обычно находятся в диапазоне $95,000 - $135,000 в зависимости от опыта.
Сопроводительное письмо
I am writing to express my strong interest in the Propulsion Engineer II position for the Archimedes Engine Systems. With a solid background in aerospace engineering and hands-on experience in rocket engine development, I am eager to contribute to Rocket Lab's mission of opening access to space through the innovative Neutron program. My technical expertise in fluid dynamics, thermodynamics, and cryogenic systems aligns perfectly with the requirements for developing next-generation propulsion hardware.
Throughout my career, I have demonstrated the ability to lead complex projects, from initial design and analysis to rigorous testing and flight operations. I am particularly drawn to Rocket Lab's fast-paced, "clean sheet" development environment and the challenge of optimizing reusable liquid launch vehicles. I am confident that my proactive approach and commitment to engineering excellence will make me a valuable asset to the Archimedes team as we push the boundaries of what is possible in space exploration.
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Откликнитесь в rocketlab уже сейчас
Присоединяйтесь к команде Rocket Lab и внесите свой вклад в создание многоразового двигателя Archimedes для ракеты Neutron!
Описание вакансии
ABOUT ROCKET LAB
Rocket Lab is an end-to-end space company delivering responsive launch services, complete spacecraft design and manufacturing, payloads, satellite components, and more – all with the goal of opening access space. 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 become the second most frequently launched U.S. rocket annually and has delivered more than 230 satellites to orbit, all while we work to develop Neutron, our upcoming medium-lift, reusable launch vehicle for larger constellation deployment. Our Space Systems business designs and builds our extensive line of satellites, payloads, and their components, including spacecraft that have been selected to support NASA missions to the Moon and Mars and components used on the James Webb Space Telescope.
NEUTRON
Neutron is a medium lift launch vehicle capable of delivering the mega constellations of tomorrow, high assurance payloads, and human spaceflight. As a highly reusable launch platform, Neutron will deliver a highly cost-effective and reliable launch solution leveraging Rocket Lab’s proven execution history with the Electron program. If you’re interested in joining a high performing team, pushing the boundaries with a clean sheet development of re-usable liquid launch vehicle, this is your opportunity!
PROPULSION ENGINEER II – ARCHIMEDES ENGINE SYSTEMS
As an Engine Systems Propulsion Engineer, you will play a critical role in the development, testing, and operation of the Archimedes Engine family, a cornerstone of the Neutron rocket program. This highly technical role involves ownership of engine subsystems, test campaigns, data analysis, and refining designs for reliability and vehicle operations, while driving system architecture trades, managing interfaces, and optimizing requirements for the vehicle.
Success requires strong autonomy, technical expertise, curiosity, attention to detail, and the ability to organize complex systems into actionable plans while collaborating across teams. You will also support engine analysis, simulation, testing, and tool development, bringing deep technical acumen to solve challenging problems. As a self-starter capable of leading projects with minimal oversight, you will have the opportunity to make a significant impact in a fast-growing startup environment that fosters growth and innovation.
WHAT YOU’LL GET TO DO:
- Design, analyze, test, fly, and refly next generation propulsion hardware ensuring operational readiness and flight success.
- Develop clear requirements and deliver validated designs and hardware that meet program milestones and flight requirements.
- Execute engine test plans, including performance validation and reliability testing, and conduct post-test data reviews to distill learnings and adjust test planning.
- Collaborate with cross-functional teams to ensure robust integration, testing, and problem solving.
- Support flight operations, including engine acceptance and post-flight analysis.
YOU’LL BRING THESE QUALIFICATIONS AS PROPULSION ENGINEER II:
- Bachelor’s degree in mechanical engineering, aerospace engineering, or related field.
- 2+ years of experience in rocket engine development, testing, or operations.
- Strong technical understanding of fluid dynamics, thermodynamics, and cryogenic systems.
- Fundamental understanding of mechanical design principles.
THESE QUALIFICATIONS WOULD BE NICE TO HAVE:
- Advanced degree in a fluid mechanics-heavy field.
- Proven ability to conduct hotfire data reviews, identify blockers for testing, and ensure operational safety of engine systems.
- Experience with staged combustion rocket engines and Methyl/LOX propellant systems.
- Background in failure analysis, combustion dynamics, turbopump mechanics, and/ or fluid systems analysis.
- Familiarity with reusable rocket engine systems and/or test/launch facility operations.
ADDITIONAL REQUIREMENTS:
- Ability to travel to our Engine Development Center (Long Beach CA) and our Launch Complex 3 (Wallops VA), approximately 25%.
- Flexibility to work extended hours or weekends as needed.
- Specific vision abilities required by this job include close vision, distance vision, peripheral vision, depth perception, and the ability to focus.
- Regularly required to sit, use hands and fingers, operate computer keyboard and controls, and communicate verbally and in writing.
- Occasional exposure to dust, fumes and moderate levels of noise.
WHAT TO EXPECT
We’re on a mission to unlock the potential of space to improve life on Earth, but that’s not an easy task. It takes hard work, determination, relentless innovation, teamwork, grit, and an unwavering commitment to achieving what others often deem impossible. Our people out-think, out-work and out-pace. We pride ourselves on having each other’s backs, checking our egos at the door, and rolling up our sleeves on all tasks big and small. We thrive under pressure, work to tight deadlines, and our focus is always on how we can deliver, rather than dwelling on the challenges that stand in the way.
Important information:
FOR CANDIDATES SEEKING TO WORK IN US OFFICES ONLY:
To conform to U.S. Government space technology export regulations, including the International Traffic in Arms Regulations (ITAR), Rocket Lab Employees must be a U.S. citizen, lawful U.S. permanent resident (i.e., current Green Card holder), or lawfully admitted into the U.S. as a refugee or granted asylum, or be eligible to obtain the required authorizations from the U.S. Department of State and/or the U.S. Department of Commerce, as applicable. Learn more about ITAR here.
Rocket Lab provides equal employment opportunities to all employees and applicants for employment and prohibits discrimination and harassment of any type without regard to race, color, religion, age, sex, national origin, disability status, genetics, protected veteran status, sexual orientation, gender identity or expression, or any other characteristic protected by federal, state or local laws. This policy applies to all terms and conditions of employment at Rocket Lab, including recruiting, hiring, placement, promotion, termination, layoff, recall, transfer, leaves of absence, compensation and training.
Applicants requiring a reasonable accommodation for the application/interview process for a job in the United States should contact Giulia Johnson at g.biow@rocketlabusa.com.This dedicated resource is intended solely to assist job seekers with disabilities whose disability prevents them from being able to apply/interview. Only messages left for this purpose will be considered. A response to your request may take up to two business days.
FOR CANDIDATES SEEKING TO WORK IN NEW ZEALAND OFFICES ONLY:
For security reasons background checks will be undertaken prior to any employment offers being made to an applicant. These checks will include nationality checks as it is a requirement of this position that you be eligible to access equipment and data regulated by the United States' International Traffic in Arms Regulations.
Under these Regulations, you may be ineligible for this role if you do not hold citizenship of Australia, Japan, New Zealand, Switzerland, the European Union or a country that is part of NATO, or if you hold ineligible dual citizenship or nationality. For more information on these Regulations, click here ITAR Regulations.
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Навыки
- Mechanical Engineering
- Aerospace Engineering
- Fluid Dynamics
- Thermodynamics
- Cryogenics
- Mechanical Design
- Data Analysis
- Failure Analysis
- Combustion Dynamics
- Turbopump Mechanics
Возможные вопросы на собеседовании
Проверка базовых знаний, необходимых для работы с ЖРД на компонентах Метан/Кислород.
Опишите основные термодинамические циклы ракетных двигателей и объясните преимущества и недостатки ступенчатого сгорания (staged combustion) для многоразовых систем.
Вакансия предполагает работу с криогенными компонентами.
С какими основными проблемами вы сталкивались при проектировании или эксплуатации криогенных систем и как вы их решали?
Важная часть роли — анализ данных после огневых испытаний.
Расскажите о вашем опыте проведения hotfire тестов: как вы интерпретируете аномалии в данных давления и температуры в реальном времени?
Двигатель Archimedes проектируется как многоразовый.
Какие конструктивные особенности наиболее критичны для обеспечения многоразовости жидкостного ракетного двигателя?
Оценка способности кандидата работать в условиях неопределенности стартапа.
Приведите пример ситуации, когда вам приходилось принимать техническое решение при неполных исходных данных или в условиях сжатых сроков.
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