Cradle Requirements Engineer

• Tasks Description:
– Requirements Engineer to provide traceability documentation and support development of verification and validation documentation. Engineer will support the Orion Spacecraft subsystems within the Crew Module Integrated Product Team. Specifically, the Environmental Controls and Life Support system, the Crew Health Habitation and Accommodation subsystem and the Passive Thermal Control subsystem. Candidate shall have working knowledge and experience in Cradle requirements management system. Tasks include, but are not limited to, the following:
– The Engineer will be responsible for development and maintenance of 3SL Cradle and associated tools/programming; and act as the local technical interface to the LM Cradle administrator in Houston
– Implement the use of Cradle Document Publisher and maintain templates to support Orion ECLSS and Crew Systems requirements and verification component/procurement spec development and configure tools to assist in configuration control for Project Orion EM-1 spec completion and EM-2 component/procurement spec generation and development
– Ensure parent traceability top-to-bottom and bottom-to-top for component spec requirements. Work capability/tools for requirements verification gap analysis. Ensure all component requirements are linked to all data items (verification reports, analyses, etc.)
– Set up and maintain the capability to Develop reports for requirements gap analysis between LM and vendor(s) requirements for fabrication/build of flight hardware including verification closure tracking/evidence
– Help to develop and maintain the capability to produce formal verification and validation documentation, preferably using Cradle Document Publisher
– Leverage work already done interfacing DOORS to Cradle for controller/software requirements traceability and to enable gap analysis
– The Contractor shall be embedded with the subsystem Team in Houston to aid in daily requirements management tasks.
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• Qualifications and Desired Skills:
– Bachelor's degree in mechanical or electrical engineering from an accredited college/university and a minimum of five years' experience in developing/working with the NASA JSC spaceflight hardware. This includes developing and maintaining requirements in Cradle and using Cradle Document Publisher (generally considered a level 3 or 4 engineer)
– Working experience with using Cradle and other associated tools to produce the exhibits detailed above. Knowledge of engineering and applicable experience with interfacing to mechanical and electrical engineers to help produce viable specifications, including requirements, for the development/fabrication of flight hardware. Experience in project and systems engineering from start to completion including the melding of ConOps, requirements, verification and validation for system and subsystem flight hardware
– Skills to ensure ConOps, System Requirements, Verification and Validation Plans are consistent with bridging to NASA standard SE practices. Experience with Microsoft Access and Virtual Basic and experience in using an SQL database
– Experience risk management tools to support requirements risk analysis and impacts on design, fabrication and schedules.
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