BEDEK. IAI.
Reassign a passenger Boeing 767 to air-fueling airplane.
Fueling pod to wing attachment, strengthening the wing structure.
A loitering munition anti-radiation drone. Composite materials structure. Aeroelastic analyses. Dynamic – flutter and divergence, static – aerodynamic coefficients.
Aeroelastic analyses to support installation of the guidance kit on a combat jet.
ORBIT. Avionics RADOME installed on Indian UAV – RUSTOME II. A whole 3 meters long composite materials canopy.
Urban Aeronautics.
Revolutionary flight vehicle. Manned. VTOL.
Structural analysis. Loads. Composite materials.
Dynamic aeroelastic analysis – Flutter
Static Aeroelasticity – Trim analysis. Influence on aerodynamic coefficients. Divergence. Loads.
MABAT, IAI.
Structural analyses for a satellite structure. Substantiation report.
VTOL UMV equipped with 3 tilted engines for VTOL and a thrust nose engine. Structural analyses and aeroelastic analyses.
Silver Arrow
Aeroelasticity and structural analyses for the UMV family of HERMES.
Structural analyses and aeroelasticity. A versatile long range UMV.