Senior Rocket propulsion engineer for MIURA 1

  • Full Time
  • AEROSPACE
  • SPAIN
  • Posted 1 week ago
  • This position has been filled
  • September 17, 2021

Company Details

Payload Aerospace, S.L (PLD Space) - Boosting the small satellite industry. e develop launch technologies to provide commercial orbital and suborbital access services , dedicated to small payloads and small satellites.

Responsibilities

  • To Participate in the TEPREL-B Liquid Rocket Engine Flight Qualification, including hardware integration, testing and post-hot test data processing.
  • To be part of the engineering decision process of MIURA 1 propulsion subsystem final development, testing and integration.
  • To provide inputs for TEPREL-B liquid rocket engine upgrades and to improve its performance.
  • To contribute and participate in the engineering decision process of MIURA 1 propellant feed system (including piping, valves, sensing, actuators, etc.)
  • To contribute in material characterization, material selection and to generate specification for updates and further developments.
  • To develop test plans for liquid propulsion parts and assemblies.
  • To generate manufacturing and assembly specifications.
  • To contribute in the upgrade PLD Space Propulsion Test Bench software and hardware.
  • To operate Company´s test bench during hot test campaigns.
  • To provide launch and mission operations support.

 

About TEPREL-B Engine

  • TEPREL-B engine has been developed internally by PLD Space, being the first liquid propellant rocket engine developed by the company.
  • This engine, fed by Kerosene and LOX in a Pressure-fed cycle has been designed to boost MIURA 1 rocket into space.
  • TEPREL-B engine has a Thrust (SL) of 32.3 KN in Sea Level and 39.7 KN in Vacuum conditions.
  • The engine is currently under Flight Qualification Process at PLD Space´s propulsion testing facilities in Teruel (Spain).
  • This engine has been developed with Spanish CDTI support in several R&D projects as well as internal company investment.

Required competences

  • Master´s degree in Aerospace Engineering.
  • Relevant experience in liquid propulsion (+7 years of liquid propulsion experience, design and testing) .
  • +5 years experiencein Finite Element Analysis using industry tools such as ANSYS.
  • Excellent use of Siemens NX/Teamcenter, EcosimPro, Matlaband Simulink tools.
  • Relevant experience in manufacturing processes (metal machining): Copper Alloys, Aluminium Alloys and Stainless-steel Alloys, as well as Electrical Discharge Machining (EDM).
  • Other relevant experience in manufacturing processes, such as Aluminium and Stainless-steel TIG Welding.
  • Good communications skills, including C1 English Level (both written and oral).
  • Ability and willingness to thrive in a fast-paced work environment.
  • Highly motivated and committed to improvement.
  • Ability to represent a workgroup.
  • Ability to work as a part of a team.

Valued competences

  • Use of Labview is desired.
  • Experience with space launch vehicle design.
  • Spanish (both written and oral).
  • Experience working with Spanish Government or National Agencies (NASA, CNES or DLR).
  • Experience working with Institutional Contracts with European Space Agency (ESA).

Experience

  • +7 years of liquid propulsion experience, design and testing

Trial Period

  • 3 months

 

Tagged as: Launcher Propulsion, Aircraft Propulsion, Cryogenic (LOX) manipulation

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