ADV000CO3 Portable Life Support System Project/Test Engineer (A)

Aerodyne Industries•Houston, TX

3d•Onsite

About The Position

Aerodyne Industries is seeking a qualified candidate for the role of Portable Life Support System (PLSS) Project/Test Engineer. This position involves performing project engineering functions for EVA spacesuit design, development, procurement, manufacture, test, and certification. The role requires working in a team environment to analyze customer requirements and develop design solutions, as well as updating plans and agreements for PLSS work scope with team leadership. The engineer will be responsible for designing, developing, testing, implementing, and analyzing technical products and systems, including designing equipment, assembling test configurations, and testing PLSS hardware. Additionally, the role involves assisting with troubleshooting technical issues, reviewing engineering drawings and specifications for compliance with NASA standards, and contributing to documentation such as test reports, hazard analyses, design reviews, and procedures.

Requirements

Bachelor's degree in Engineering with experience in the field or in a related area.
BS degree in engineering from an accredited engineering school.
Excellent oral and written communication skills.
Ability to work in a team environment.
Resumes, in month and year format, must be submitted with application in order to be considered for the position.

Nice To Haves

Detailed knowledge of vent loop gas flow rates, pressure management, and PLSS outlet CO2 control in closed loop and open loop modes.
Detailed knowledge on xEMU selected design goals for each vent loop component, including design and purpose, pressure capabilities, flow rates/delta pressure during flow, and functional operations.
Understanding of previous vent loop build/manufacturing issues and testing including component checkouts and DVT/TVAC testing.
Ability to describe the consequences of making various design alterations to the existing xEMU baseline design.
Detailed knowledge of thermal control and auxiliary thermal control loops including heat removal capabilities, pressures and flow rates, water/loop materials compatibility, and issues with extended quiescent stowage.
Detailed knowledge of design trades that led to the selection of xEMU thermal loop component designs, hardware design, and hardware build/manufacturing history including issues encountered and resolution.
Knowledge of testing including component checkouts and PLSS level DVT/TVAC testing.
Ability to describe the consequences of making various design alterations to the existing xEMU baseline design.
Experience with pressure systems including relief valves, pressure transducers, flow meters, and the calibration process of each is preferred.

Responsibilities

Perform project engineering functions for EVA spacesuit design, development, procurement, manufacture, test, and certification.
Work in a team environment to analyze requirements from customers and develop design solutions.
Work with the PLSS Team leadership to update plans and agreements for PLSS work scope.
Design, develop, test, implement, and analyze technical products and systems.
Design equipment, design and assemble test configurations and complete testing of PLSS hardware.
Assist with troubleshooting and resolving technical issues identified during testing and integration.
Review engineering drawings, requirements, and system specifications to ensure accuracy and compliance with NASA standards.
Contribute to documentation, including test reports, hazard analyses, design reviews, procedures and TPS creation and execution.