Designed various structural components for the launch site.Performed fluid analysis calculations for the helium, nitrous and nitrogen systems. Applying an understanding of gaseous, liquid, and two phase flow. Designed nitrous oxide fill system including analysis, conceptual and detailed design of the filling mechanism.Designed helium recovery system including analysis, conceptual and detailed design of the recovery mechanism.Updated launch site P&ID.Produced drawings for various piping manifolds, sheet metal parts, welded assemblies, etc.Made operational procedures for helium recovery and N2O systems.

Re-design of data acquisition and control system for a hybrid rocket engine testing facility, as well as a ground support electrical system for the rocket oxidizer filling system.

Research on sizing of hybrid rocket combustion chamber to optimize performance. Designed various sub-components of the launch rail as well as managing assembly tests for the system.