Periodic Reporting for period 1 - RETALT (Retro Propulsion Assisted Landing Technologies)
Reporting period: 2019-03-01 to 2020-02-29
During the three years of the project lifetime the consortium will investigate the areas of aerodynamics, aerothermodynamics (i.e. the temperatures that evolve at the surface of the vehicle during flight), flight dynamics, guidance, navigation and control, and advanced structural parts, materials and mechanisms. For this purpose, two types of rocket launchers will be investigated which both start and land in an upright position. Up to now, orbital heavy lift rockets are only used once. This is one of the reasons for high launch costs. Landing a rocket and reusing it afterwards has the potential of big cost savings. One of the rockets investigated will have two stages and will be similar to conventional rockets like the Falcon 9 or the Ariane 5 launcher. For this launcher only the first stage will be landed again. The second launcher has only a single stage. It will be designed for the use of smaller payloads and when returning it will break not only with retro propulsion but also with the aid of a large aerodynamic base surface at the bottom.
These rockets will not really be launched; however, they will be used as the reference configurations for the investigations of the different technologies in the project. Aerodynamic wind tunnel experiments, numerical simulations and ground tests of several components will serve to verify the outcomes of the project.
The objective of the project is to raise the Technical Readiness Level (a measure of 1 to 9 of how far a technology is away from market readiness) up to 5 for most of the technologies investigated in the project and up to 3 for the Guidance and Navigation and Control system. This means that the technologies will be demonstrated in a representative environment and can be tested in prototypes in a next step. The partners strive for concepts of reusable launch vehicle that best combine all the investigated technologies in a single design, in view of a demonstration in orbit in follow-up projects.
The project started in March 2019; the progress of the project can be followed on: www.retalt.eu
With the defined reference rockets, work started on the structural design of the landing legs and the wings (or aerodynamic control surfaces) which are needed to steer the rockets to the ground and land them safely. At the same time, investigations were performed on the thermal protection system (TPS) for the forward facing base plate of the rockets, on a mechanism to steer the landing rockets with the engines (TVC) and on a control system for the landing approach. Furthermore, the aerodynamic characterization of the rockets was refined.
Research activities in space (e.g. on the ISS) are also directly influenced by the space transportation costs. This research is crucial for the society, as it is often directly related to human lives (e.g. in space medicine). By reducing costs for space research, RETALT directly contributes to better lives for the European citizens.
By lowering costs of space transportation and therefore for space technologies and research, RETALT contributes to ensures a globally competitive and innovative European space sector, by making it easier for companies and start-ups to access space data as it becomes more affordable. Thus, it directly contributes to the European competitiveness and growth in the space industry and related sectors.