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מעל 90,000 משרות • אלפי משרות חדשות בכל יום
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כבר העליתם קו"ח בעבר? כניסה
מלאה
22,000-35,000 ₪
Required Composite Structures Engineer
Why this role exists
The airframe is not just a load path - it is part of the acoustic system. Every panel that vibrates radiates, every joint that transmits structure-borne energy undoes work the rest of the vehicle did to stay quiet. You will design and substantiate the composite structure of a novel lift and propulsion architecture where laminate stiffness, ply-level damping, and transmission-path isolation are traded as deliberately as mass and strength - because our roughly fourfold acoustic advantage survives only if the structure carries it.
What you'll own:
Design composite primary and secondary structure - laminate definitions, ply schedules, core selections, bonded and bolted joints - from concept layout through released engineering definition.
Build, run, and own detailed FEA models for static strength, buckling, and structural dynamics, and keep them correlated against coupon, element, and full-scale test evidence.
Drive vibro-acoustic behavior of the airframe: characterize panel modal density, radiation efficiency, and structure-borne transmission paths, and turn stiffness and damping into deliberate acoustic design levers.
Define and execute structural test campaigns - building-block coupon and element tests, modal surveys and ground vibration tests - including instrumentation plans, test readiness reviews, and post-test model correlation.
Develop material allowables and laminate design values with materials and process engineers, and document the basis for every margin you claim.
Write structural substantiation reports with traceable loads, methods, and margins of safety that will stand up to a certification authority, not just an internal review.
Trade mass against transmission loss and damping treatments directly with the Acoustics team, and defend the structural side of those trades at vehicle-level design reviews.
Support the build: assess layup and tooling feasibility, review first articles, and disposition manufacturing discrepancies on flight hardware.
Why this role exists
The airframe is not just a load path - it is part of the acoustic system. Every panel that vibrates radiates, every joint that transmits structure-borne energy undoes work the rest of the vehicle did to stay quiet. You will design and substantiate the composite structure of a novel lift and propulsion architecture where laminate stiffness, ply-level damping, and transmission-path isolation are traded as deliberately as mass and strength - because our roughly fourfold acoustic advantage survives only if the structure carries it.
What you'll own:
Design composite primary and secondary structure - laminate definitions, ply schedules, core selections, bonded and bolted joints - from concept layout through released engineering definition.
Build, run, and own detailed FEA models for static strength, buckling, and structural dynamics, and keep them correlated against coupon, element, and full-scale test evidence.
Drive vibro-acoustic behavior of the airframe: characterize panel modal density, radiation efficiency, and structure-borne transmission paths, and turn stiffness and damping into deliberate acoustic design levers.
Define and execute structural test campaigns - building-block coupon and element tests, modal surveys and ground vibration tests - including instrumentation plans, test readiness reviews, and post-test model correlation.
Develop material allowables and laminate design values with materials and process engineers, and document the basis for every margin you claim.
Write structural substantiation reports with traceable loads, methods, and margins of safety that will stand up to a certification authority, not just an internal review.
Trade mass against transmission loss and damping treatments directly with the Acoustics team, and defend the structural side of those trades at vehicle-level design reviews.
Support the build: assess layup and tooling feasibility, review first articles, and disposition manufacturing discrepancies on flight hardware.
Requirements:
What you bring
B.Sc. in Aerospace or Mechanical Engineering; M.Sc. with a structures or structural dynamics focus preferred.
5+ years designing and analyzing composite airframe or primary structure on aircraft, rotorcraft, UAS, or comparable flight vehicles.
Strong hands-on FEA capability in Nastran, ANSYS, or Abaqus across statics, buckling, and dynamics - with demonstrated correlation of models to physical test data.
Solid command of classical laminate theory, composite failure criteria, and the design of bolted and bonded joints in laminated structure.
Working fluency in structural dynamics: modal analysis, frequency response, and damping characterization, and an understanding of how these connect to radiated noise.
Experience carrying structure through physical test - static, fatigue, or modal/GVT - from test planning and instrumentation through post-test reporting.
Proficiency in Python or MATLAB for analysis automation, data reduction, and test-data processing.
Fluency in 3D CAD (CATIA, NX, or SolidWorks) and GD&T, with the ability to release production-ready structural definition.
Even better if:
Composite airframe experience on an eVTOL, UAM, or light aircraft program, especially during the prototype-to-flight-test phase.
Hands-on use of vibro-acoustic analysis tools such as Actran or VA One, or statistical energy analysis methods.
Exposure to composite structural substantiation under CS-23/Part 23 or rotorcraft rules, including familiarity with AC 20-107B practice.
A track record of owning structure at startup pace - from blank sheet to hardware on a test stand in months, not years.
Publications or graduate research in structural acoustics, damped composite design, or vibration transmission in built-up structures.
What you bring
B.Sc. in Aerospace or Mechanical Engineering; M.Sc. with a structures or structural dynamics focus preferred.
5+ years designing and analyzing composite airframe or primary structure on aircraft, rotorcraft, UAS, or comparable flight vehicles.
Strong hands-on FEA capability in Nastran, ANSYS, or Abaqus across statics, buckling, and dynamics - with demonstrated correlation of models to physical test data.
Solid command of classical laminate theory, composite failure criteria, and the design of bolted and bonded joints in laminated structure.
Working fluency in structural dynamics: modal analysis, frequency response, and damping characterization, and an understanding of how these connect to radiated noise.
Experience carrying structure through physical test - static, fatigue, or modal/GVT - from test planning and instrumentation through post-test reporting.
Proficiency in Python or MATLAB for analysis automation, data reduction, and test-data processing.
Fluency in 3D CAD (CATIA, NX, or SolidWorks) and GD&T, with the ability to release production-ready structural definition.
Even better if:
Composite airframe experience on an eVTOL, UAM, or light aircraft program, especially during the prototype-to-flight-test phase.
Hands-on use of vibro-acoustic analysis tools such as Actran or VA One, or statistical energy analysis methods.
Exposure to composite structural substantiation under CS-23/Part 23 or rotorcraft rules, including familiarity with AC 20-107B practice.
A track record of owning structure at startup pace - from blank sheet to hardware on a test stand in months, not years.
Publications or graduate research in structural acoustics, damped composite design, or vibration transmission in built-up structures.
This position is open to all candidates.
במקום לעבור לבד על אלפי מודעות, Jobify מנתחת את קורות החיים שלך ומציגה לך רק משרות שבאמת מתאימות לך.
מעל 90,000 משרות • אלפי משרות חדשות בכל יום
חינם. בלי פרסומות. בלי אותיות קטנות.
DOCX, DOC, PDF - בעברית או באנגלית
כבר העליתם קו"ח בעבר? כניסה
משרות נוספות מומלצות עבורך
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חיפה
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קרית גת
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נשר
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מהנדס בניין בתחום קונסטרוקציה
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באר שבע
אור הנדסה
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מהנדס /ת בניין /מהנדס /ת אזרחי
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ראשון לציון
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מהנדס /ת קונסטרוקציה- תכנון מערכות חיפוי מבנים
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פתח תקווה
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ערב
36 חודשים
תעודה ממשלתית
סבסוד
חיפה
