Mid-Level Structural Loads and Dynamics Analyst at Boeing Grant, AL
The Boeing Defense, Space & Security (BDS), Boeing Space & Launch Engineering is seeking a highly motivated Mid-Level Structural Loads and Dynamics Analyst (Level 3) to support the Huntsville Loads and Dynamics manager across various Programs in Huntsville, AL.
The Space Launch System (SLS) program (primary program supported), in conjunction with NASA, is developing the nation's capability in manned access to space, including destinations beyond Earth orbit.
Position Overview:
This position independently performs loads development, integration, and documentation of advanced structural analysis across multiple Boeing Development Systems (BDS) programs, including the SLS Program and Commercial Crew.
This position will perform detailed finite element modeling and coupled loads analysis for the Exploration Upper Stage.
You will be responsible for generating design loads in pursuit of the overall design, development, and test of hardware.
This is not a union represented position.
Position
Responsibilities:
Directly supports the Huntsville Alabama Loads and Dynamics Flight Capability leader across multiple programs and several sites.
Conducts analysis processes independently, in consultation with more senior engineers, to support loads analyses.
Loads analysis includes independent simulations using NASTRAN of all ground and flight events to which the launch vehicle is exposed, and the development of internal loads on secondary structures or components associated with these flight events.
Examples include liftoff, ascent (gust/buffet response), and base-drive analysis using NASTRAN, etc.
Performance of loads and dynamics analysis to assure compliance with structural integrity and stability requirements, taking guidance from the Technical Lead.
Analysis, test, and certification of space flight hardware designs for NASA's Space Launch Systems, Exploration Upper Stage (EUS).
Leadership will include tasking and oversight of junior and senior analysts.
Method selection, tools, and technical authority will be developed.
Customer contact and coordination will be instrumental and a critical skill for the successful candidate.
Hardware includes cryogenic, pressurized and unpressurized structure, propulsion delivery systems, mechanisms and mechanical systems.
Production support is also performed.
Some travel may be required, includes the production facility in New Orleans, test houses and suppliers in various states.
Work Authorization:
This position requires ability to obtain program access, for which the U.
S.
Government requires U.
S.
Citizenship.
This position requires the ability to obtain access to a National Aeronautics and Space Administration (NASA) facility.
Access to the facility requires a background investigation by U.
S.
Government authorities.
Basic Qualifications (Required Skills/Experience):
Bachelor, Master or Doctorate of Science degree from an accredited course of study, in engineering, computer science, mathematics, physics or chemistry.
2 or more years of experience using MATLAB or similar language environment to develop analytical tools or perform numerical modeling of complex systems.
2 or more years of experience in launch vehicle loads development.
Experience using NASTRAN and PATRAN finite element modeling software.
Preferred Qualifications (Desired Skills/Experience):
2 or more years of experience in generating launch vehicle Craig-Bampton Models and performing Coupled Loads Analysis.
1 or more years of experience in creating launch vehicle Load Transformation Matrices (LTM) for aerospace applications.
Experience with structural dynamic analysis and/or FEA based loads developmentExperience in dynamic test planning and test data evaluation for launch vehicles.
Experience with loads development for NASA or Air Force programs.
Experience on space, launch vehicle, and/or aircraft programs.
Experience in NASA Space programs or a related Space or Defense programTypical Education/
Experience:
Education/experience typically acquired through advanced technical education from an accredited course of study in engineering, computer science, mathematics, physics or chemistry (e.
g.
Bachelor) and typically 5 or more years' related work experience or an equivalent combination of technical education and experience (e.
g.
PhD, Master+3 years' related work experience).
In the USA, ABET accreditation is the preferred, although not required, accreditation standard.
Relocation:
This position is located in a location that does not offer relocation.
Candidates must live in the immediate area or relocate at their own expense.
Drug Free Workplace:
Boeing is a Drug Free Workplace where post offer applicants and employees are subject to testing for marijuana, cocaine, opioids, amphetamines, PCP, and alcohol when criteria is met as outlined in our policies.
.
Estimated Salary: $20 to $28 per hour based on qualifications.
The Space Launch System (SLS) program (primary program supported), in conjunction with NASA, is developing the nation's capability in manned access to space, including destinations beyond Earth orbit.
Position Overview:
This position independently performs loads development, integration, and documentation of advanced structural analysis across multiple Boeing Development Systems (BDS) programs, including the SLS Program and Commercial Crew.
This position will perform detailed finite element modeling and coupled loads analysis for the Exploration Upper Stage.
You will be responsible for generating design loads in pursuit of the overall design, development, and test of hardware.
This is not a union represented position.
Position
Responsibilities:
Directly supports the Huntsville Alabama Loads and Dynamics Flight Capability leader across multiple programs and several sites.
Conducts analysis processes independently, in consultation with more senior engineers, to support loads analyses.
Loads analysis includes independent simulations using NASTRAN of all ground and flight events to which the launch vehicle is exposed, and the development of internal loads on secondary structures or components associated with these flight events.
Examples include liftoff, ascent (gust/buffet response), and base-drive analysis using NASTRAN, etc.
Performance of loads and dynamics analysis to assure compliance with structural integrity and stability requirements, taking guidance from the Technical Lead.
Analysis, test, and certification of space flight hardware designs for NASA's Space Launch Systems, Exploration Upper Stage (EUS).
Leadership will include tasking and oversight of junior and senior analysts.
Method selection, tools, and technical authority will be developed.
Customer contact and coordination will be instrumental and a critical skill for the successful candidate.
Hardware includes cryogenic, pressurized and unpressurized structure, propulsion delivery systems, mechanisms and mechanical systems.
Production support is also performed.
Some travel may be required, includes the production facility in New Orleans, test houses and suppliers in various states.
Work Authorization:
This position requires ability to obtain program access, for which the U.
S.
Government requires U.
S.
Citizenship.
This position requires the ability to obtain access to a National Aeronautics and Space Administration (NASA) facility.
Access to the facility requires a background investigation by U.
S.
Government authorities.
Basic Qualifications (Required Skills/Experience):
Bachelor, Master or Doctorate of Science degree from an accredited course of study, in engineering, computer science, mathematics, physics or chemistry.
2 or more years of experience using MATLAB or similar language environment to develop analytical tools or perform numerical modeling of complex systems.
2 or more years of experience in launch vehicle loads development.
Experience using NASTRAN and PATRAN finite element modeling software.
Preferred Qualifications (Desired Skills/Experience):
2 or more years of experience in generating launch vehicle Craig-Bampton Models and performing Coupled Loads Analysis.
1 or more years of experience in creating launch vehicle Load Transformation Matrices (LTM) for aerospace applications.
Experience with structural dynamic analysis and/or FEA based loads developmentExperience in dynamic test planning and test data evaluation for launch vehicles.
Experience with loads development for NASA or Air Force programs.
Experience on space, launch vehicle, and/or aircraft programs.
Experience in NASA Space programs or a related Space or Defense programTypical Education/
Experience:
Education/experience typically acquired through advanced technical education from an accredited course of study in engineering, computer science, mathematics, physics or chemistry (e.
g.
Bachelor) and typically 5 or more years' related work experience or an equivalent combination of technical education and experience (e.
g.
PhD, Master+3 years' related work experience).
In the USA, ABET accreditation is the preferred, although not required, accreditation standard.
Relocation:
This position is located in a location that does not offer relocation.
Candidates must live in the immediate area or relocate at their own expense.
Drug Free Workplace:
Boeing is a Drug Free Workplace where post offer applicants and employees are subject to testing for marijuana, cocaine, opioids, amphetamines, PCP, and alcohol when criteria is met as outlined in our policies.
.
Estimated Salary: $20 to $28 per hour based on qualifications.
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