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Area: SYSTEM ENGINEERING AND AVIONICS

System Engineer

SITE: Elche
TYPE: Full time (3 months trial)
REFERENCE: V214

Description

  • Systems Engineer for MIURA 1 launch vehicles and associated tests and future launch operations.

 

Responsibilities

  • Develop and manage system and subsystem requirements, including verification techniques and interface control.
  • Work proactively and collaboratively with the engineering team and customer to identify, track, mitigate, and resolve technical/programmatic issues that may arise during program execution.
  • Serve as engineering focal for mission requirements and exchange of technical information between subsystems on launch vehicles and payloads.
  • Assist with the development of design, integration, and test processes, procedures, and configurations for launch vehicles in concert with other engineering disciplines.
  • Provide support for design/analysis results level to technical team and program management.
  • To be part of launch vehicle Simulation analysis and other performance analysis across vehicle functions.
  • To assist with the development of test methods and plans according to defined requirements.
  • To be part of CONOPS upgrade and implementation.
  • To elaborate design documents.

Required competences

  • Master's degree in Aerospace engineering, Electrical Engineering, Mechanical Engineering, Systems Engineering or equivalent.
  • +3 years’ experience with Systems Engineering SW tools
  • +3years experience in high reliability Systems Engineering design and processes
  • +2 years’ experience with space systems, satellite, launch vehicles, etc.
  • Experience managing technical budgets, requirements, V&V, AIT and plan definition
  • Expertise in Computer Aided Design (CAD) using industry tools such as Siemens NX.
  • Ability to work with multidisciplinary teams in technical and programmatic areas
  • Experience with space Launch Vehicle (suborbital or orbital)
  • Familiarity with hardware test program requirements captured in industry standards including ESA ECSS Standards, SMC-S-016, NASA-STD-7001, NASA-STD-7002 and GSFC-STD-7000.
  • Team player able to work with different subsystems

Valued competences

  • Experience with mission definition and requirements
  • Experience in environmental testing, thermal vacuum, vibration, electromagnetic compatibility, as well as test methods and validation.
  • Expertise in Matlab/Phyton.
  • Understanding of launch vehicle key subsystems and their associated performance parameters.
  • Experience in managing subcontractors.
  • Fast adaptability to rapid changes environments.

Experience

  • Experience working with government, NASA, ESA or commercial launch contracts.
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hhrr_214@pldspace.com

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