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This research addresses critical flight contingencies for Virgin Galactic's SpaceShipTwo (SS2) suborbital vehicle to analyze and evaluate the feasibility of its flight operations. The research suborbital data was obtained using the Embry-Riddle Aeronautical University Suborbital Space Flight Simulator. These suborbital flight profiles were simulated after drop from WhiteKnightTwo for several contingency scenarios, such as ontrajectory failures (thrust termination), fuel dumping, loss of vector control, and tumbling turn failures. The simulated data obtained from these flights will be used as a preliminary step for future developments of flight planning to better estimate the space flight corridors during descent and ascent trajectories, which will provide flight and ground safety operators with key information to better understand hazard and safety risks and establish pertinent procedures and preventive measures when the vehicle goes through the National Air Space (NAS). Problems of interest as outlined by the Federal Aviation Administration 1 : • Altering the launch or reentry trajectory, to the extent possible, to avoid placing airspace restrictions in congested airspace.