ADV000CO2 Portable Life Support System Project Engineer (A)

Aerodyne Industries•Houston, TX

3d•Onsite

About The Position

Aerodyne Industries is seeking a Portable Life Support System (PLSS) Project Engineer to join their team. This role involves performing project engineering functions for EVA spacesuit design, development, procurement, manufacture, test, and certification. The engineer will work in a team environment to analyze customer requirements and develop design solutions, update plans and agreements for PLSS work scope, and design, develop, test, implement, and analyze technical products and systems. This includes designing equipment, assembling test configurations, and completing testing of PLSS hardware. The position also requires assisting with troubleshooting and resolving technical issues, and reviewing engineering drawings, requirements, and system specifications for accuracy and compliance with NASA standards. Contribution to documentation, including test reports, hazard analyses, design reviews, procedures, and TPS creation and execution, is also expected.

Requirements

Bachelor's degree in Engineering and a minimum of 2-5 years of experience in the field or in a related area.
BS degree in engineering from an accredited engineering school and minimum 3 years experience.
Excellent oral and written communication skills.
Ability to work in a team environment.

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 detailed understanding of each component's 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, issues with extended quiescent stowage.
Detailed knowledge of design trades that led to the selection of xEMU thermal loop component designs, detailed knowledge of hardware design, knowledge of xEMU thermal loop hardware build/manufacturing history including issues encountered and resolution, and knowledge of testing including component checkouts and PLSS level DVT/TVAC testing.
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.