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Avionics CAD Assembly
MIL-STD-810 & DO-160 Qualification of Ruggedized Avionics Systems
TEN TECH LLC provides structural & thermal analysis services to qualify ruggedized designs to MIL-STD-810 and RTCA/DO-160 specifications, including:
  • Thermal System-Level Modeling
  • Detailed Finite Elements Modeling, directly from 3D CAD assembly
  • Random, shock and sine vibration response Finite Elements Analysis
  • Board-level solder joint fatigue and system fatigue life prediction
  • Detailed CFD & thermal analysis: component junction and card edge temperatures
  • Environmental Stress Screening (ESS) test plan, per MIL-HDBK-2164
  • ESS physical test for thermal shock and sine-on-random
Electronics Cooling CFD Thermal
Chassis NASTRAN Random Shock Vibration
Spacecraft Systems Dynamics & Thermal Analysis
TEN TECH LLC provides analysis support for spacecraft antenna and bus systems, including:
  • Finite Element Modeling, from 3D CAD models
  • Natural frequencies and normal modes
  • Random vibration response analysis
  • Transportation and launch shock analysis
  • Vibro-Acoustics response
  • Fatigue and Cumulative Damage Analysis
  • On-orbit Radiation Thermal Analysis
  • Range of Motion Kinematics Analysis
  • Deployment Flexible Body Mechanisms Analysis
  • Thermal Vacuum Chamber physical test
  • Combined Random & Thermal environment test
Spacecraft Mechanism Motion Kinematics ADAMS Recurdyn
Vibroacoustics VAOne NASTRAN
SRS DDAM Pyroshock Random Shock
Waveguide Sress FEA NASTRAN