Airframe Structures Dynamics Engineer

Airframe Structures Dynamics Engineer

Location: Palmdale, CA

Job ID: #69445

12 month contract

SECRET clearance

Pay Range: $100-120

Lockheed Martin Aeronautics in seeking a full-time Airframe Structures Dynamics Engineer for the Advanced Development Programs (ADP) in Palmdale, California. A successful candidate will apply technical expertise in developing solutions to aircraft structural design problems. Responsibilities for this position may include:

• Creation and/or modification of primary and secondary structural parts, assemblies, installations, and interface control models/documents.

• Contributing to developing, testing, and validating aircraft structural dynamics analyses.

• Assisting in creating system requirements, trade studies, statements of work, and test plans.

• Coordination with internal Integrated Product Teams (IPTs), with some interaction with external IPTs and suppliers.

Basic Qualifications :

• Bachelor's degree in an engineering technical discipline such as Mechanical, Aerospace, or Aeronautical; 9 years experience with a Bachelor's Degree or 7 years with a Master's Degree

• Experience making/updating Finite Element Models (FEM) in Patran, Hypermesh, FEMAP, or similar

• Experience with running and interpreting Modal Analysis (SOL103), Random Vibration (SOL111), Transient Analysis (SOL112), Non-linear analysis (SOL106/400)

• Experience with developing vibration environments for aircraft (Mission Based Analysis) and maintaining Environment Criteria Documents (ECD)

• Experience with vibroacoustic and data processing

• Subsystem qualification experience (vendor testing, interpreting previous qualification data and making assessment to current predicted environments, delta qual, etc.)

• Proficient in scripting language (MatLab, Python, VBA, C++, etc.)

• Experience with documenting technical results and analysis and presenting to customers in an effective way

Desired skills :

• Proficient in MSC/Hexagon ADAMs for mechanism and landing gear

• Familiar with RCC-319

• Experience with structural analysis for preliminary sizing

Required skills:

• Bachelor's degree in an engineering technical discipline such as Mechanical, Aerospace, or Aeronautical; 9 years experience with a Bachelor's Degree or 7 years with a Master's Degree

• Experience with running and interpreting Modal or frequency Analysis for example: (SOL103), Random Vibration (SOL111), Transient Analysis (SOL112), Non-linear analysis (SOL106/400)

• Experience with developing vibration environments for aircraft (Mission Based Analysis) and maintaining Environment Criteria Documents (ECD) of MIL- STD 810

• Experience with vibroacoustic and data processing

• Experience making/updating Finite Element Models (FEM) in Patran, Hypermesh, FEMAP, or similar

• Previous experience in a scripting language (MatLab, Python, VBA, C++, etc.)

• Subsystem qualification experience (vendor testing, interpreting previous qualification data and making assessment to current predicted environments, delta qual, etc.)

Benefits provided: 401K, medical, dental, and vision, sick time as applicable to state law

Butler America Aerospace, LLC. is proud to provide an equal opportunity workplace and be an affirmative action employer. Consider Butler because we are committed to hiring and retaining a diverse workforce. We recognize that we thrive on diversity and inclusion for the benefit of our employees, our customers, and the communities where we are located. Employment decisions are made without regard to race, color, religion, gender, national origin, ethnicity, veteran status, disability status, age, sexual orientation, gender identity, gender expression, marital status, mental or physical disability or any other legally protected status.