Utilizing experimental / computational aerodynamic database, Zeus Numerix provides services in the areas of flight dynamics, particularly,

• Trajectory Profile: Utilizing its 3 and 6 DOF modules, Zeus Numerix has proven expertise in estimation of spinning rocket & missile trajectories. Either of the experimental or computational aerodynamic databases can be utilized for this purpose.



Trajectory of rocket in Boost Phase

Trajectory of rocket in Ballistic Phase
• Stage Separation: Services are offered for the most crucial maneuvers a space vehicle undertakes during the mission. The aerodynamic interference between two separating objects is understood and demonstrated for hypersonic program.



Stage Separation of the Cruiser Vehicle from the Launch Vehicle
• Store Separation: Integrated CFD, 6 DOF analysis is offered to ensure perfect separation of aircraft store.


• Aerodynamic Control Surface: Zeus Numerix has been delivering databases related to aerodynamic response to changes of the deflection angle of control surfaces.