nivel 5

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
Senior Liquid Rocket Propulsion Development Engineer for MIURA 1 and MIURA 5 Launch Vehicle.

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 experience in Finite Element Analysis using industry tools such as ANSYS.
Excellent use of Siemens NX/Teamcenter, EcosimPro, Matlab and 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.

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
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
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.

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 analysis and architecture of pressure-fed liquid rocket engine, including component sizing, loads determination, and detailed analysis.
Perform thermal / mechanical load analysis for propellant lines (including cryogenics and fuel lines as well as high pressure gas lines).
Create and manage test and development plans for engines and propulsion components.
Perform analysis and interpretation from Propulsion test and flight data.
Generation of Engineering documentation.
Maintain and improve program standard approaches to analysis.
Liaise with Design Engineers of the same department and with others Engineering departments (Structures design and stress, M&P, Quality, etc.) and provide information to the Manufacturing area under request.
Continuous research to optimize analysis 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 analysis metallic structures for propellant lines.
Knowledge in selection and application of analysis criteria according to the loading conditions, working environment, etc.
Fluent written and oral communication both in Spanish and English

Valued competences
Previous experience in Aerospace Industry as Propulsion analysis engineer or Stress Analysis Engineer (or an equivalent combination of education and experience).
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.
Familiar with Aerospace standard parts and typical light materials, metallic and non-metallic.
Preferred software: Ansys 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.

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.

Nivel 7

nivel 7

nivel 7

Description
As part of a small, passionate, and accomplished team, you will be responsible for designing the control hardware of ground infrastructures such as test benches and launch pad systems in concert with Mechanical departments

Responsibilities
Control hardware design of test benches for validate components and subsystems of launchers MIURA 1 and MIURA 5
Control hardware design of MIURA 5 launch pad
Responsible to accomplish with specifications and requirements during the development of the assigned tasks
Responsible of hardware control system design along the entire lifecycle and across all phases from Design, Manufacturing and Commissioning.
Liaise with Mechanical department for accomplish operational requirements of developed facilities
Generation of Engineering documentation such as Electric Drawings, BOMs, and Eng. Change Notes for the complete definition of Electric Cabinets, Sensors, and Actuators.
Participate in 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 test benches and launch pad functionalities
Complete the assigned tasks “on time, on quality, on cost"

Required Knowledge
Automation, Electrical or Electronic Engineering Bachelor’s degree or demonstrable relevant experience in lieu thereof
> 5 years of relevant technical experience
Demonstrated experience in design automation systems for industrial machinery and electrical commissioning of industrial lines
Knowledge in selection and application of design criteria and rules, wires, connectors, and other electrical properties according to the project requirements
Preferred automation hardware knolled: Nation Instrument and Beckhoff

Required competences
Fluent written and oral communication both in Spanish and English.
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

Valued competences
Passionate and creative problem solver that thrives in fast-paced environment
Understanding of other disciplines: mechanical, fluids management, LabView development…

Others
Travels: Teruel, Huelva
Image 1

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 3

PROPULSION ANALYSIS ENGINEER
Subtipos:
TP Analysis
TCA Analysis
Propulsion Analysis (general)
Eco SIMPRO

Nivel 3

PROPULSION DESIGN ENGINEER
Subtipos:
TP Design
TCA Design
Piping Design
Harness Design

Nivel 3

Nivel 7

Under the Program Management team, we're looking for a Document Management Specialist who will work along with the both engineering and operation teams in order to organize and control the documentation needed to be elaborated.

Responsabilities
Write, review, implement and execute plans for new or established document management system, policies and procedures regarding document elaboration, approval, storage, sharing, transmission, and destruction.
Elaborate documentation template for technical documents and operational documents (i.e. technical review documents, program management documents, test reports, test plans, integration procedures, Requirements specifications, …)
Follow, track and evaluate team documentation implementation activities and elaborate plannings and track deadlines for technical documentation releasing.
Evaluate existing document management systems and procedures to determine current effectiveness and efficiency; identify and recommend improvements.
Consults with engineering and operations teams to identify problems in accessing electronic content.
Ensures security of system and integrity of master documents by implementing document and system access rights and revision controls.
Ensures company complies with applicable laws and regulations regarding data security and document management.
Maintains current knowledge of best practices and developments in document management technologies and techniques through participation in monthly Program Review meetings.

Required Knowledge
Technical Bachelors degree, engineering preferred.
At least 5 years of related experience required.

Required Competences
Perfect communication skills.
Microsoft Office Suite
Organizational skills and attention to detail.
Basic understanding of laws and regulations regarding document management.
Analytical and technical skills.
Problem-solving skills.

Desired Competences
Aerospace industry knowledge or interests
Previous experience with technical docummentation

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.