Description
Trajectory design and analysis of launch vehicles and related launch operations in the department of Systems and GNC.

Responsibilities
Perform trajectory design, optimization, and dispersion for suborbital and orbital launch vehicles.
Development of 6-DOF launch vehicle and spacecraft dynamics simulators.
Perform aerodynamic characterization of aerospace vehicles.
Contribute to flight safety analysis, safety corridors, IIPs.
Interaction with other subsystems and systems engineers for trajectory optimization.
Contribution to launch licensing according to international regulations.
Provide inputs for flight hardware (structural and propulsion components).
Pre-flight / post-flight data processing and correlation with simulations and tests.
Software verification via testing with flight-software-in-the-loop and hardware-in-the-loop.

Required competences
Master's degree in Aerospace engineering, Space exploration or flight mechanics, or GNC.
5-7 years of experience with Matlab/Simulink.
5-7 years of experience with flight simulation programs (rocket trajectories) and orbital mechanics.
Experience with space Launch Vehicle trajectory simulations (suborbital or orbital) and with the use of ASTOS, STK or similar software.
Relevant experience in rocket trajectory analysis and simulation software development.
Knowledge of Computer Fluid Dynamics (CFD) software.
Knowledge of ballistic missile and orbital trajectory simulations
Knowledge of aerodynamic reentry simulations and analysis
Knowledge of security analysis and international regulations
English
Stress Tolerance
Problem solving
Multitasking
Wordload capacity
Autonomy

Valued competences
Experience with spacecraft orbital trajectory design and simulations.
Experience with ballistic missile trajectory design.
Experience with re-entry aerothermodynamics analysis and simulations.
Experience with Safety analysis and international regulations for launch vehicles.
Experience with FTS design and dispersion simulation.
Experience with control dynamics and optimization strategies for missile and orbital spacecrafts.

Equal Employment Opportunity
Payload Aerospace SL is an equal opportunity employer and does not discriminate against gender, marital status, religion, age, colour, race, sexual orientation, nationality or disability.
We are compromised in maintaining a diverse and free from discrimination working environment where everyone is treated with respect. Employment is based on an individual’s merit and qualifications, directly related to job competence.
These principles are included in all aspects of employment: recruiting, hiring, training, compensation and benefits, and promotion.

Description
PLD Space is seeking a new member for our team to serve as Propulsion test engineer for MIURA 1 and MIURA 5 launch vehicle. The primary role of this position involves testing hardware from development, qualification, and acceptance for flight at both subsystem and component level. The Candidate will carry out rocket engine testing activities and propulsive stage testing activities at PLD Space propulsion facilities in Teruel (Spain). This role is for a hands-on person. The main workplace will be Elche with frequent travels to Teruel and Huelva.

Responsibilities
Deep understanding of liquid rocket engine propulsion subsystems and components.
Deep understanding of test procedures, industry standards, and best-practices.
Knowledge of thermodynamic principles as applied to cryogenics and high-pressure systems, to ensure test facilities can provide physical parameters defined for each engine system or component.
Knowledge of safety principles and best practices while working with high pressure fluids and cryogenics.
Perform fundamental fluid flow, heat transfer and structural analysis to contribute to the design and development of new propulsion test facilities
Write test plans, test procedures, and maintain configuration management system.
Perform data analysis and prepare data reviews and performance reports to evaluate propulsion test facility performance.
Work with technicians in the field to prepare test articles prior to testing.
Coordinate with technicians to operate cryogenic facilities, fuel facilities and high-pressure lines for engine testing.
Provide support to System Engineering department to define, coordinate and control the functional and physical interfaces between the propulsion system and the launch vehicle.
Perform other duties as assigned.

Required competences
BSc in Aerospace Engineering or Mechanical Engineering.
Must be able to stand for extended periods.
Must be able to maneuver in tight spaces.
Must be able to handle items weighting more than 15kg.

Valued competences
Experience working with high pressure systems, desired experience with Fuel and/or cryogenic components and propellants.
Knowledge of manufacturing processes, test & integration procedures of liquid aerospace propulsion systems or pressurized system.
Experience
5+ years of Rocket Propulsion subsystem testing activities or aerospace-related propulsion testing activities.

Equal Employment Opportunity
Payload Aerospace SL is an equal opportunity employer and does not discriminate against gender, marital status, religion, age, colour, race, sexual orientation, nationality or disability.
We are compromised in maintaining a diverse and free from discrimination working environment where everyone is treated with respect. Employment is based on an individual’s merit and qualifications, directly related to job competence.
These principles are included in all aspects of employment: recruiting, hiring, training, compensation and benefits, and promotion.

Description
PLD Space is seeking a new member for our team to serve as a Test Engineer, within the Structures Department. This position will be focused on assisting the qualification, and acceptance testing of structural components for its launch programs

Responsibilities
Definition of tests, considering available inputs, requested outputs and measurements, as well as other boundary conditions.
Test campaign planning.
Test suppliers management: contact, evaluation, selection, agreements.
Test execution/follow-up.
Assessment of externally executed tests.
Assistance in post-processing of test data in collaborations with Stress team.
Report writing and internal dissemination of test outcomes.
Assessment of sensorization requirements and load conditions for which data is to be obtained in order to meet test objectives in a safe manner.
Collaborate in the design of test benches and tooling.
Create work methodologies or improve the existing ones in order to benefit current and future projects.
Research state of the art in testing methodologies and sensors and propose creative approaches to complex problems.
Occasionally travel to other PLD Space or supplier locations.

Required competences
Aerospace or Mechanical Engineer.
Fluency in English is mandatory.
+5 years’ experience in similar position, testbench/hardware and lab work.
Used to work with standards (ECSS, ISO, EN, ASTM, MIL...).
Used to work under pressure without neglecting safety and quality.
Strong analytical and problem-solving skills, along with excellent written and oral communication skills.

Valued competences
Knowledge on specific space sector, space vehicles and launchers, metallic pressure vessels, COPV and payload structures is high desirable.
Knowledge of pressure vessel codes (BPVC, EN 13345, PD5500, AD 2000...).
Skills on electronics, optical instrumentation and extensiometric measurement will be welcomed.
Vibration and dynamic analysis test experience.
Experience in analysis or design positions is desirable.
Experience with Catia or NX Unigraphics is desirable.
Basic knowledge of finite element analysis shall be welcomed.
Programming experience (Matlab/Octave, Python...) is desirable.
Experience
Experience developing and conducting test plans for experimental structural test.
Knowledge on developing reports to analyse test results from test execution.
Experience working with testbenches.


Equal Employment Opportunity
Payload Aerospace SL is an equal opportunity employer and does not discriminate against gender, marital status, religion, age, colour, race, sexual orientation, nationality or disability.
We are compromised in maintaining a diverse and free from discrimination working environment where everyone is treated with respect. Employment is based on an individual’s merit and qualifications, directly related to job competence.
These principles are included in all aspects of employment: recruiting, hiring, training, compensation and benefits, and promotion.

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.

Equal Employment Opportunity
Payload Aerospace SL is an equal opportunity employer and does not discriminate against gender, marital status, religion, age, colour, race, sexual orientation, nationality or disability.
We are compromised in maintaining a diverse and free from discrimination working environment where everyone is treated with respect. Employment is based on an individual’s merit and qualifications, directly related to job competence.
These principles are included in all aspects of employment: recruiting, hiring, training, compensation and benefits, and promotion.

Description
As part of a small, passionate, and accomplished team, you will be responsible for designing launch vehicle Propulsion elements and configurations in concert with Structures subsystem. Specific focus on Propellant lines design.

Responsibilities
Participate in subsystem design and architecture of pressure-fed liquid rocket engine, including component sizing, loads determination, and detailed design.
Design of primary metallic structures (different size range of machined components, sheet metal parts) for propellant lines (cryogenics, fuel and gas) fitting.
Design of secondary structures as brackets or supports for rigid pipes, valves, mechanism, propulsion components electrical harness, etc.
Generation of Engineering documentation such as 3D models, Drawings, BOMs, and Eng. Change Notes for the complete definition of Detailed Parts, Assemblies, and Installation.
Maintain and improve program standard approaches to design, safety factors, material allowables, drafting standards, etc.
Liaise with others Engineering departments (Structures design and stress, M&P, Quality, etc.) and provide information to the Manufacturing area under request.
Responsible to accomplish with specifications and requirements during the development of the assigned tasks or product design along the entire lifecycle and across all phases from Prototype, Testing and Series production.
Participate in the periodic design reviews dealing with SCH/Manufacturing for the achievement of requirements, specifications, feasibility, lead time and prices.
Continuous research to optimize design solutions.
Identify and recommend opportunities to reduce costs and improve efficiency.
Complete the assigned tasks “on time, on quality, on cost".

Required competences
Aerospace or Mechanical Engineering Bachelor’s degree or demonstrable relevant experience in lieu thereof.
Minimum 3 years of relevant technical experience.
Demonstrated experience in design metallic structures for propellant lines.
Knowledge in selection and application of design criteria and rules, materials, strengths, and other mechanical properties, according to the loading conditions, working environment, etc.
High degree of CAD competence and PDM tools.
Fluent written and oral communication both in Spanish and English

Valued competences
Previous experience in Aerospace Industry as Propulsion design & analysis engineer or Structural Design Engineer (or an equivalent combination of education and experience).
Familiar with Aerospace standards
Familiar with the main manufacturing technologies and capabilities
Knowledge of the most common corrosion prevention rules and surface protection.
Knowledge of the most common cryogenic (LOX) cleaning procedures.
Knowledge of Cryogenic (LOX) manipulation.
Proven in the development of products from the original concept design according to Aerospace normative and rules, through to the delivery of detailed technical design packaging into final production.
Design focused to assembly line concerns, tooling, and jigs.
Familiar with Aerospace standard parts and typical light materials, metallic and non-metallic.
Preferred software: Siemens NX and Teamcenter.
An occasional need to travel with the role will be required.
Self-motivated and able to work under pressure to meet deadlines, dealing with situations that are constrained by time and managing different tasks at once.
Able to work autonomously with little supervision.

Equal Employment Opportunity
Payload Aerospace SL is an equal opportunity employer and does not discriminate against gender, marital status, religion, age, colour, race, sexual orientation, nationality or disability.
We are compromised in maintaining a diverse and free from discrimination working environment where everyone is treated with respect. Employment is based on an individual’s merit and qualifications, directly related to job competence.
These principles are included in all aspects of employment: recruiting, hiring, training, compensation and benefits, and promotion.

Nivel 6

Description
En PLD Space estamos buscando a jóvenes inquietos, interesados en la industria espacial y con muchas ganas de aprender.
Si estás interesado en realizar prácticas curriculares o extracurriculares de grado y máster de cualquier titulación, déjanos aquí tu CV.

Please, be aware that Young Talent Programss works as a data base to keep your contact details. It is not an open and active recruitment process.
We will review your CV and only in case we have an opportunity that fits with your profile, we will contact you.