Design Engineer
Apply NowCompany: RIT Solutions, Inc.
Location: San Mateo, CA 94403
Description:
REQUIRED QUALIFICATIONS:
Minimum education of a Bachelor's degree in Aeronautical engineering with credentials.
Min 10 - max 20 years' of direct Engineering design experience, in the spacecraft or aerospace industry, with project ownership.
5-10 years working experience with classical hand stress analysis methods.
Experience in technical report writing and must have excellent communication skills, be fluent in English (spoken and written) and proficient in MS Word, MS Excel, MS Teams.
Must be able to work effectively in a team environment.
Design work starting at the conceptual level, maturing into full 3D modeling, validation with FEA analysis and hand calculations, and continuing into manufacturing.
Possess in-depth knowledge of and applicable experience with aircraft structural analysis methods, including hand calculation experience for mechanical joints. Using resources such as MMPDS, Bruhn, Roark, etc., aircraft fasteners, materials, sheet metal assemblies, machined fittings.
Experience with the structural and fatigue analysis of mechanical and electronic components. System and component level static, vibration, acoustic, modal, shock test experience with aerospace flight hardware.
Appropriate Knowledge of regulatory (F nd/or military) issues related to aircraft design and analysis and their impact on conformity and compliance is required (i.e., certification, qualification).
You must provide evidence of proficiency in performing advanced stress analysis capability using NASTRAN and finite element modeling.
Minimum education of a Bachelor's degree in Aeronautical engineering with credentials.
Min 10 - max 20 years' of direct Engineering design experience, in the spacecraft or aerospace industry, with project ownership.
5-10 years working experience with classical hand stress analysis methods.
Experience in technical report writing and must have excellent communication skills, be fluent in English (spoken and written) and proficient in MS Word, MS Excel, MS Teams.
Must be able to work effectively in a team environment.
Design work starting at the conceptual level, maturing into full 3D modeling, validation with FEA analysis and hand calculations, and continuing into manufacturing.
Possess in-depth knowledge of and applicable experience with aircraft structural analysis methods, including hand calculation experience for mechanical joints. Using resources such as MMPDS, Bruhn, Roark, etc., aircraft fasteners, materials, sheet metal assemblies, machined fittings.
Experience with the structural and fatigue analysis of mechanical and electronic components. System and component level static, vibration, acoustic, modal, shock test experience with aerospace flight hardware.
Appropriate Knowledge of regulatory (F nd/or military) issues related to aircraft design and analysis and their impact on conformity and compliance is required (i.e., certification, qualification).
You must provide evidence of proficiency in performing advanced stress analysis capability using NASTRAN and finite element modeling.