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FLPP

Future Launchers Preparatory Program

ANED-M

The project was focused on statistical fitting of model parameters to measurements, identification of worst case scenario and geometry optimisation and its goal was to propose a methodology for optimisation of nozzle extension geometry so as to minimise its weight and maximise its reliability with respect to the prescribed uncertain loading.

Polymeric liner

The goal of the project, which was run in close cooperation with EADS CASA, was to develop sufficiently effective barrier based on thermosetting polymers. It would be used on future generations of reusable launch vehicles in effort to reduce the overall vehicle weight.

FLUTTER

The goal of the project was flutter assessment of jettisonable versatile thermal insulation panels of upper cryogenic stage of a launcher.

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