Composite engine thrust frame design and manufacturing using fibre steering optimization for launcher structures
Composite engine thrust frame design and manufacturing using fibre steering optimization for launcher structures
Date
2021
Authors
Brink, W.M. van den
Maas, R.
Gerrits, W.
Journal Title
Journal ISSN
Volume Title
Publisher
Netherlands Aerospace Centre NLR
Abstract
New space launcher systems from ESA will enter a very competitive commercial launcher market. New entrants to this
market have reduced the launch price per unit mass payload by half (50%). As a consequence a key requirement for
the development of new launchers is reduced recurring production costs and increased performance.
A part of the space launcher is the Engine Thrust Frame (ETF), also known as the ViTF (Vinci Thrust Frame). This
research was done under lead of Airbus Defense and Space Netherlands and funded by ESA. In line with the launcher’s
key requirements the main goal of this research is to save recurring production costs, lower the weight and keep the
stiffness requirements of the composite ViTF structure using different innovative design and stiffening techniques,
such as fibre steering.
The Carbon Fibre Reinforced Plastic (CFRP) full scale reference thrust frame was used as a starting point. Design and
optimization of the thrust frame composite layup using the fibre steering method is performed to reduce weight and
meet the mechanical requirements. This was followed by detailed analyses and evaluation of the design. For testing
purposes the full scale design was scaled down to 1:3 scale. This 1:3 design is manufactured and tested.
The optimisation of the full-scale thrust frame design and 1:3 scaled version leads to a significant reduction in weight
of 15% compared to the Carbon Fibre Reinforced Plastic (CFRP) reference design. This is achieved by reduction of the
amount of blade stiffeners and introduction of the automated fibre steering which results in a more optimal design.
The requirements for safety, strength and stiffness are still met with the new design. The optimisation efforts resulted
in a design that reached ultimate load without failure and buckling.
The tools and methods developed enable next generation composite structures using laminate optimization and fibre
steering.