Objective
Objects re-entering the atmosphere of the Earth from space require systems to decelerate the object during its descent phase as well as protection against temperatures of several hundreds of degrees of centigrade caused by the atmospheric friction. We propose to study the feasibility of using with the Earth re-entry a system developed for entering the Martian atmosphere. The focus of this work will be in analyzing and measuring the dynamical stability in transonic phase of a brand new re-entry and descent system for low mass payloads.
We are to investigate an entry, descent and landing system developed for Mars. This system is based on brand new technology involving inflatable structures saving a considerable amount of mass compared to traditional rigid structures. The project behind is MetNet Precursor, which is a planetary exploration mission to Mars, aimed to deploy on its surface a meteorological station based on a new type of semi-hard landing vehicle called MetNet Lander (MNL).
This work will investigate the feasibility to use the MetNet entry and descent system at Earth allowing for scaling modifications for the key systems assuming deorbitation from a LEO orbit. Specifically, this work will analyze by simulations and by wind tunnel testing the stability of the entry and descent system during the supersonic and transonic phases of the descent in the atmosphere of the Earth.
This work will foster collaboration between Russian and European organizations, and will provide brand-new knowledge on the re-entry systems. This project will effectively reduce duplication of research efforts and will open new avenues for joint space technology research and development.
Fields of science (EuroSciVoc)
CORDIS classifies projects with EuroSciVoc, a multilingual taxonomy of fields of science, through a semi-automatic process based on NLP techniques. See: The European Science Vocabulary.
CORDIS classifies projects with EuroSciVoc, a multilingual taxonomy of fields of science, through a semi-automatic process based on NLP techniques. See: The European Science Vocabulary.
- engineering and technology mechanical engineering vehicle engineering aerospace engineering aircraft
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Programme(s)
Multi-annual funding programmes that define the EU’s priorities for research and innovation.
Multi-annual funding programmes that define the EU’s priorities for research and innovation.
Topic(s)
Calls for proposals are divided into topics. A topic defines a specific subject or area for which applicants can submit proposals. The description of a topic comprises its specific scope and the expected impact of the funded project.
Calls for proposals are divided into topics. A topic defines a specific subject or area for which applicants can submit proposals. The description of a topic comprises its specific scope and the expected impact of the funded project.
Call for proposal
Procedure for inviting applicants to submit project proposals, with the aim of receiving EU funding.
Procedure for inviting applicants to submit project proposals, with the aim of receiving EU funding.
FP7-SPACE-2010-1
See other projects for this call
Funding Scheme
Funding scheme (or “Type of Action”) inside a programme with common features. It specifies: the scope of what is funded; the reimbursement rate; specific evaluation criteria to qualify for funding; and the use of simplified forms of costs like lump sums.
Funding scheme (or “Type of Action”) inside a programme with common features. It specifies: the scope of what is funded; the reimbursement rate; specific evaluation criteria to qualify for funding; and the use of simplified forms of costs like lump sums.
Coordinator
00560 Helsinki
Finland
The total costs incurred by this organisation to participate in the project, including direct and indirect costs. This amount is a subset of the overall project budget.