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Wing-design algorithm based on modified linear theory taking into account effects of attainable leading-edge thrust. Provides analysis as well as design capability and applicable to both subsonic and supersonic flow.
Create Augmented Reality (AR)/Virtual Reality (VR) tools for integrating spacecraft designs and real-time mission telemetry for multiple domains over a mission lifecycle: Pre-phase A concept design Hardware integration & test planning and execution Tele-robotic operations
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