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Propulsion Design Engineer (m/f/d)
Исключительная возможность в сфере New Space с отличным пакетом льгот (акции, пенсия, обучение) и участием в разработке реальной ракеты-носителя.
Сложность вакансии
Высокая сложность обусловлена необходимостью глубоких знаний в термодинамике, архитектуре ракетных двигателей и стохастическом анализе, а также междисциплинарным характером роли.
Анализ зарплаты
Предлагаемая роль инженера в аэрокосмической отрасли Германии обычно оплачивается в диапазоне 65,000–85,000 евро в год в зависимости от опыта. Isar Aerospace является конкурентоспособным работодателем, предлагающим дополнительные бонусы в виде виртуальных акций.
Сопроводительное письмо
I am writing to express my strong interest in the Propulsion Design Engineer position at Isar Aerospace. With a solid background in aerospace engineering and a deep fascination with engine cycle calculations, I am eager to contribute to the development of the Spectrum launch vehicle. My experience in developing analytical models for complex fluid systems aligns perfectly with your need for precise engine load point predictions and performance uncertainty quantifications.
Throughout my academic and professional career, I have developed a profound understanding of thermodynamics and rocket motor architecture. I am particularly drawn to Isar Aerospace's mission to democratize space access and would welcome the opportunity to collaborate with the Turbopump and GNC teams to ensure the highest standards of engine performance. I am confident that my technical skills in Simulink and stochastic analysis, combined with my proactive approach, will make me a valuable asset to your propulsion department.
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Описание вакансии
Mission Brief
As Propulsion Design Engineer with focus on engine cycle calculations you will be responsible for the implementation of engine models to provide load point predictions, engine performance uncertainty quantifications, and serve as the main person of contact to the Guidance Navigation and Control Team to provide engine performance models and parameters for the flight software. You will be working within the Turbopump Team and collaborate with system owners of all subcomponents of the engine.
Your Role in Our Space Mission
Key responsibilities within the Turbopump Team:
- Develop and maintain modular engine models of existing engines and fluid systems as well as conceptual engines in the development phase for engine load point predictions and performance studies.
+ Coordinate with product owners and ensure model characterization of every subcomponent of the engine and maintain component performance database.
+ Provide load point predictions during development and test campaigns and define acceptance criteria for flight engines / qualification tests with respect to engine performance.
- Serve as the main point of contact to provide engine performance metrices for the flight software to Guidance Navigation Controls and conduct uncertainty quantification for such metrices.
+ Maintain database of characteristic parameters such as Isp and mass flow as well as lookup tables for engine transients.
+ Maintain secondary engine models relevant for rocket kinematics in all phases of the mission such as thrust generated by chill down bleed flows, purges etc.
+ Conduct conceptional engine performance studies in early development of future launch systems or iterations of Spectrum.
- Ensure consistent data acquisition quality of engine performance parameters in development testing, stage testing and flight.
+ Define Sensor requirements for in flight performance verification of the engines.
+ Elaborate uncertainty propagation of the entire measurement chain in collaboration with test rig responsibles to maintain a high data quality standard.
Qualification Checklist
- M.Sc. degree in mechanical engineering, aerospace engineering or similar.
- Exceptional knowledge in thermodynamics and rocket motor system architecture as well as sub system interactions.
- Knowledge in measurement technology and stochastic analysis (Uncertainty Quantification and propagation).
- Fundamental understanding of combustion, thrust chambers, valves and turbopump systems.
- Proven experience in developing and validating empiric, semi empiric or analytical models as well as setting up cycle models of complex fluid systems/machinery
- Effective collaborator in multi-disciplinary and cross-functional teams, organized, detail-oriented, and proactive. Ability to adapt to shifting priorities.
- Driven and eager to learn, passionate about new space, fluent in English
Bonus Skills
- Professional work experience in rocket propulsion development.
- Working experience in Simulink or cycle model development in rocket/aircraft engines or similar
- Willingness to travel to support engine test campaigns and launch campaigns abroad.
Benefits
- Employee Participation Program: Share in our success through our virtual company share program
- 30 days of vacation: Enjoy the days off to relax and recharge
- Company pension plan: Secure your future with our company pension plan, featuring a 20% employer contribution after the probation period
- Subsidised lunch: Stay energised with delicious, subsidised lunches every day
- Public transport ticket: Commute with ease using a fully financed Deutschlandticket
- Sport Clubs membership: Stay fit with our sponsored sports club memberships (EGYM Wellpass)
- Individual learning allowance: Grow your skills with an individual learning budget granted after the probation period
- Childcare allowance: Receive a childcare allowance for your non-school-age children
- And Much More! Discover additional perks and benefits when you join our team
Who we are
We are Isar Aerospace and we are at the forefront of New Space building a modern space business to enable faster, better and cheaper access to space.
Our mission is to help democratise space and use it for good in order to improve life on Earth now and for the future generations.
We are a fast-growing company aiming to provide sustainable and environmentally friendly launch solutions for small and medium-sized satellites and constellations into Low Earth Orbit. The company is privately funded by world-leading technology investors with strong commitment and support and our team is made of driven and talented people with a real passion for space innovation.
We're making rockets in a way that hasn't been done before disrupting a traditional industry. If you are up for the challenge, want to work on cutting-edge projects and be part of a team changing the world for better, come, join us and launch your career!
Want to find out more about us?
Visit www.isaraerospace.com
Disclaimer
Isar Aerospace SE is an equal-opportunity employer committed to fairness and inclusivity. We do not prioritize any specific religion, gender, nationality, or background. Due to security clearance requirements, affiliations with countries listed under § 13 para. 1 no. 17 SÜG may affect the application process. All qualified applicants are encouraged to apply.
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Навыки
- Thermodynamics
- Simulink
- Aerospace Engineering
- Propulsion Systems
- Fluid Systems
- Stochastic Analysis
- Uncertainty Quantification
- Rocket Engines
- Mechanical Engineering
Возможные вопросы на собеседовании
Проверка фундаментальных знаний, критически важных для расчета циклов двигателя.
Опишите процесс моделирования термодинамического цикла ЖРД и то, как вы учитываете потери в различных компонентах системы.
Роль требует тесного взаимодействия с командой GNC.
Как вы подходите к передаче данных о производительности двигателя команде управления и навигации (GNC) для интеграции в полетное ПО?
В описании вакансии упоминается важность оценки неопределенностей.
Какие методы вы используете для количественной оценки неопределенности (Uncertainty Quantification) в моделях производительности двигателя?
Проверка практических навыков работы с инструментами моделирования.
Расскажите о вашем опыте работы в Simulink или аналогичных средах для моделирования переходных процессов в жидкостных системах.
Оценка способности работать в условиях реальных испытаний.
Как вы определяете требования к датчикам для верификации характеристик двигателя во время полета и наземных тестов?
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