Applications
Aerospace
- Building high fidelity structural finite element models
- Booster/launch pad separation transients
- Booster/payload integrated transient event coupled loads analyses (CLA)
- Booster/payload integrated nonlinear transient event CLA incorporating dead-band clearances, friction, foam properties, nonlinear dampers, snubbers, ...
- Booster/payload integrated transient event variational (sensitivity) CLA
- Booster/payload integrated transient event CLA incorporating time-varying mass
- Booster staging event analyses and fairing separation analyses
- Booster/payload integrated quasi-static flight event analyses
- Payload transient loads analyses with detailed internal payload recoveries
- Spacecraft docking analyses
- Booster/payload integrated random vibration event analyses: liftoff acoustics and transonic
- Component random vibration analysis including environment mitigation due to component mass attenuation
- System and component level testing and analysis correlation
- Analytic integration of complex systems into single reduce dynamic math models
- Reduction of finite element math models to dynamic math models
- Independent verification and validation of associate contractors’ work
For more information, please contact ASD.