Senior structural analysis and test support for aerospace payloads and defense systems — from concept through qualification.
Southern California · Supporting Programs Nationwide
Structural work is treated as a connected system — loads, models, design decisions, test environments, and correlation are developed together.
Analysis is built around the decisions it needs to support. Models are structured to answer specific program questions, close margins, and withstand external review.
Work is documented and traceable, with a clear technical basis that can be carried into design reviews, test planning, and customer interface without rework or reinterpretation.
The same engineer develops the analysis, supports the decisions, and interfaces with customers, integrators, and review boards — maintaining continuity from initial definition through test and correlation.
Real programs rarely follow a clean analytical path. Models that are technically correct can still produce the wrong answer when load paths are uncertain, interfaces are non-kinematic, or behavior depends on assembly.
A significant portion of structural engineering work is recognizing when that condition exists — and resolving it without unnecessary redesign or iteration.
Structural support for aerospace payloads, optical instruments, and precision systems where alignment stability, interface sensitivity, and qualification environments drive the design from the start.
Primary structure in aerospace is predominantly composite — solid laminate, honeycomb sandwich, and bonded joints. CSD supports programs where composite structure is the baseline, not an exception, from early sizing through margin closure and test.
Nonlinear structural analysis for deployable systems — reflector deployment, hinged mechanisms, and hardware with contact, large displacement, or sequential load path changes. Executed using advanced FEM solvers where linear assumptions break down.
Structural analysis and test support through the qualification and acceptance cycle — test readiness reviews, fixture design, instrumentation, execution support, and test-analysis correlation. Work is structured so the analytical basis is defensible at QRB and doesn’t require reconstruction when the program needs to move.
Finite element model development from early idealization through load cycle participation, margin closure, integrator handoff, and test correlation. Models are structured to support the full analytical lifecycle.