United States-Virginia-Dulles, United States
$81-151k
Full Time
an hour ago
Job description
Description
At Northrop Grumman, our employees have incredible opportunities to work on revolutionary systems that impact people's lives around the world today, and for generations to come. Our pioneering and inventive spirit has enabled us to be at the forefront of many technological advancements in our nation's history - from the first flight across the Atlantic Ocean, to stealth bombers, to landing on the moon. We look for people who have bold new ideas, courage and a pioneering spirit to join forces to invent the future, and have fun along the way. Our culture thrives on intellectual curiosity, cognitive diversity and bringing your whole self to work — and we have an insatiable drive to do what others think is impossible. Our employees are not only part of history, they're making history.Embark on a career putting innovative, reliable, and agile products and ideas into orbit, and beyond. Northrop Grumman has opportunities waiting for you that play a vital role in human space exploration, national defense, and scientific discovery, supporting multiple programs across the universe. With us, you’ll discover a culture of curiosity and collaboration that will have you Defining Possible from the day you start. Our space systems connect and protect millions of people on earth every day, now and for the future. Explore your future and launch your career today.
The Tactical Space System Mechanical Engineering organization is seeking a mid to senior level Mechanical/Structural Analysis Engineer to assist an experienced team of mechanical engineers performing mechanical and structural analysis on one or more spacecraft systems or subsystems.
Responsibilities may include the following:
Performing static and dynamic structure analysis.
Reviewing requirements for materials, structure systems & subsystems.
Selecting appropriate technical information and data from applicable products.
Determining the technical principles involved, identifying the design path forward and computing the engineering characteristics to ensure consistency with the specifications design needs and requirements of space applications.
Releasing results as “technical documents” after review by the senior members of the team.
Developing innovative solutions and elaborating on design concepts.
Evaluating completed designs with supervisor and other technical groups, and making modifications necessary to achieve the most ideal design.
This requisition may be filled at a higher grade based on qualifications listed below.
Basic Qualifications:
This requisition may be filled at a either a Mechanical Structural Engineer or Principal level.
Basic Qualifications for Principal Mechanical/Structural Engineer 2:
Bachelor’s degree in STEM - Science, Technology, Engineer, Math or related area (Mechanical Engineering or Degrees with a focus in Structural Analysis highly preferred) 2+ years of experience OR a Master’s Degree.
Ability to perform structural engineering tasks associated with analysis, design, and/or testing of structures.
Experience with at least one of the following Mechanical Analysis tools such as NX FEMAP/NASTRAN, ABAQUS, HYPERMESH. (Equivalent spacecraft structural analysis tools may be considered on a case by case basis).
Active TS security clearance at time of application
Basic Qualifications for Principal Mechanical/Structural Engineer 3:
Bachelor’s degree in STEM - Science, Technology, Engineer, Math or related area (Mechanical Engineering or Degrees with a focus in Structural Analysis highly preferred) 5+ years of experience, Master’s Degree and 3+ years, OR a PhD.
Ability to perform structural engineering tasks associated with analysis, design, and/or testing of structures.
Experience with at least one of the following Mechanical Analysis tools such as NX FEMAP/NASTRAN, ABAQUS, HYPERMESH. (Equivalent spacecraft structural analysis tools may be considered on a case by case basis).
Active TS security clearance at time of application
Preferred Qualifications:
Experience with spacecraft or subsystem static/dynamic testing
Experience utilizing MATLAB
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