Northrop Grumman
Propulsion Engineer/Princ Propulsion Engineer - R10210949
Northrop Grumman, Corinne, Utah, United States, 84307
Propulsion Engineer – Northrop Grumman Space Systems
Location: Promontory, UT | Clearance: Secret | Relocation Assistance: Available | Travel: 10% of the time
Role Summary
Northrop Grumman Space Systems is seeking a Propulsion Engineer to join our Loaded Motor team. The Engineer will evaluate internal ballistic performance of solid rocket motors ranging from launch vehicle boosters to subscale laboratory test motors and support the design and analysis needed for future propulsion systems. Responsibilities
Analyze ground test and flight motor performance using computer software. Design solid propellant grain geometries for new rocket motors. Assess results of static tests to improve analytical modeling. Develop and present documented analyses to internal and external customers. Evaluate historical motor performance data and develop performance requirements. Coordinate tasks with other analysts and designers. Improve and update analytical methods and computer software. Perform tasks in adjacent roles such as thermal, structural, design, and CFD. Core Qualifications
Level 2
Bachelor’s degree in engineering (e.g., Aerospace, Mechanical, Chemical) and 2 years of experience, or an MS degree in engineering. Basic knowledge of solid rocket motors and their performance. Computer programming (MATLAB, FORTRAN, C, C++) and CAD proficiency. Familiarity with statistics and statistical methods. Highly self‑motivated, with excellent written and oral communication skills. Strong time‑management and organizational skills; detail oriented. Willingness to learn. Level 3
Bachelor’s degree in engineering and 5 years of experience, or an MS degree in engineering and 3 years of experience. Basic knowledge of solid rocket motors and their performance. Computer programming (MATLAB, FORTRAN, C, C++) and CAD proficiency. Familiarity with statistics and statistical methods. Highly self‑motivated, with excellent written and oral communication skills. Strong time‑management and organizational skills; detail oriented. Willingness to learn. Preferred Qualifications
Master’s or PhD in engineering (e.g., Aerospace, Mechanical, Chemical). Emphasis on rocket propulsion, combustion, fluid dynamics, or thermodynamics. Technical analysis experience and large‑data evaluation skills. Demonstrated success in a team environment. Additional Requirements
Successful candidate must be able to obtain and maintain a U.S. Government Security Clearance. Benefits
Medical, Dental & Vision coverage 401k Educational Assistance Life Insurance Employee Assistance Programs & Work/Life Solutions Paid Time Off Health & Wellness Resources Employee Discounts Northrop Grumman is an Equal Opportunity Employer, making decisions without regard to race, color, religion, creed, sex, sexual orientation, gender identity, marital status, national origin, age, veteran status, disability, or any other protected class. For our complete EEO and pay transparency statement, please visit
NorthropGrumman.com/EEO . U.S. Citizenship is required for all positions with a government clearance and certain other restricted positions.
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Northrop Grumman Space Systems is seeking a Propulsion Engineer to join our Loaded Motor team. The Engineer will evaluate internal ballistic performance of solid rocket motors ranging from launch vehicle boosters to subscale laboratory test motors and support the design and analysis needed for future propulsion systems. Responsibilities
Analyze ground test and flight motor performance using computer software. Design solid propellant grain geometries for new rocket motors. Assess results of static tests to improve analytical modeling. Develop and present documented analyses to internal and external customers. Evaluate historical motor performance data and develop performance requirements. Coordinate tasks with other analysts and designers. Improve and update analytical methods and computer software. Perform tasks in adjacent roles such as thermal, structural, design, and CFD. Core Qualifications
Level 2
Bachelor’s degree in engineering (e.g., Aerospace, Mechanical, Chemical) and 2 years of experience, or an MS degree in engineering. Basic knowledge of solid rocket motors and their performance. Computer programming (MATLAB, FORTRAN, C, C++) and CAD proficiency. Familiarity with statistics and statistical methods. Highly self‑motivated, with excellent written and oral communication skills. Strong time‑management and organizational skills; detail oriented. Willingness to learn. Level 3
Bachelor’s degree in engineering and 5 years of experience, or an MS degree in engineering and 3 years of experience. Basic knowledge of solid rocket motors and their performance. Computer programming (MATLAB, FORTRAN, C, C++) and CAD proficiency. Familiarity with statistics and statistical methods. Highly self‑motivated, with excellent written and oral communication skills. Strong time‑management and organizational skills; detail oriented. Willingness to learn. Preferred Qualifications
Master’s or PhD in engineering (e.g., Aerospace, Mechanical, Chemical). Emphasis on rocket propulsion, combustion, fluid dynamics, or thermodynamics. Technical analysis experience and large‑data evaluation skills. Demonstrated success in a team environment. Additional Requirements
Successful candidate must be able to obtain and maintain a U.S. Government Security Clearance. Benefits
Medical, Dental & Vision coverage 401k Educational Assistance Life Insurance Employee Assistance Programs & Work/Life Solutions Paid Time Off Health & Wellness Resources Employee Discounts Northrop Grumman is an Equal Opportunity Employer, making decisions without regard to race, color, religion, creed, sex, sexual orientation, gender identity, marital status, national origin, age, veteran status, disability, or any other protected class. For our complete EEO and pay transparency statement, please visit
NorthropGrumman.com/EEO . U.S. Citizenship is required for all positions with a government clearance and certain other restricted positions.
#J-18808-Ljbffr