Load Analysis & Definition: Calculate and establish static and dynamic design load cases for all flight and ground phases, including transportation, launchpad operations, engine ignition, atmospheric ascent (aerodynamic loads), staging, re-entry, and landing.
Coupled Loads Analysis (CLA): Build and execute complex mathematical simulation models by coupling launch vehicle and payload models to predict critical flight environments and transient events.
Modeling & Simulation: Develop and optimize finite element models (FEM) and perform structural dynamics analyses, including transient, sinusoidal, random vibration (PSD), gusts, and acoustic response analyses.
Testing & Validation: Design, oversee, and analyze data from physical tests (e.g., modal surveys, vibration, and shock testing) and correlate simulation models with actual flight telemetry data.
Education: University degree in Aerospace Engineering, Mechanical Engineering, or a related field with a strong focus on structural dynamics or continuum mechanics.
Experience: Proven experience in structural loads definition, structural dynamics, or aeroelasticity, ideally within the development of launch vehicles, satellites, or missiles.
Technical Skills:
Deep understanding of structural dynamics, vibe/shock environments, and acoustic phenomena.
Proficiency with commercial FEA solvers (Optistruct) and pre-/post-processors (HyperMesh).
Job details are sourced from the employer's original posting.
Open job postingAbout the company
Hypersonica is a company focused on advanced systems engineering, likely in the aerospace or defense sector, given the job description's emphasis on mission objectives, requirements decomposition, and model-based systems engineering (MBSE).