Coordinatore | DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV
Organization address
address: Linder Hoehe contact info |
Nazionalità Coordinatore | Germany [DE] |
Sito del progetto | http://www.dlr.de/as/sacomar |
Totale costo | 690˙530 € |
EC contributo | 499˙484 € |
Programma | FP7-SPACE
Specific Programme "Cooperation": Space |
Code Call | FP7-SPACE-2010-1 |
Funding Scheme | CP-FP-SICA |
Anno di inizio | 2011 |
Periodo (anno-mese-giorno) | 2011-01-01 - 2012-06-30 |
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1 |
DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV
Organization address
address: Linder Hoehe contact info |
DE (KOELN) | coordinator | 175˙745.58 |
2 |
FEDERALNOE GOSUDARSTVENNOE UNITARNOPREDPRIYATIE TSENTRALNY NAUCHNO- ISSLEDOVATELSKY INSTITUT MACHINOSTROENIYA
Organization address
address: PIONERSKAYA 4 contact info |
RU (KOROLEV) | participant | 99˙172.20 |
3 |
A. ISHLINSKY INSTITUTE FOR PROBLEMS IN MECHANICS RUSSIAN ACADEMY OF SCIENCE*IPMECH RAS
Organization address
address: PROSPEKT VERNADSKOGO 101 - Block 1 contact info |
RU (MOSCOW) | participant | 58˙500.00 |
4 |
FEDERAL STATE UNITARY ENTERPRISE THE CENTRAL AEROHYDRODYNAMIC INSTITUTE NAMED AFTER PROF. N.E. ZHUKOVSKY
Organization address
address: Zhukovsky str 1 contact info |
RU (ZHUKOVSKY) | participant | 41˙250.00 |
5 |
CENTRO ITALIANO RICERCHE AEROSPAZIALI SCPA
Organization address
address: Via Maiorise 1 contact info |
IT (CAPUA - CASERTA) | participant | 34˙862.96 |
6 |
THALES ALENIA SPACE ITALIA SPA
Organization address
address: Via Saccomuro 24 contact info |
IT (ROMA) | participant | 30˙557.20 |
7 |
AIRBUS DS GMBH
Organization address
address: ROBERT KOCH STRASSE 1 contact info |
DE (TAUFKIRCHEN) | participant | 30˙522.00 |
8 |
SA KHRISTIANOVICH INSTITUTE OF THEORETICAL AND APPLIED MECHANICS OF SIBERIAN BRANCH OF RUSSIAN ACADEMY OFSCIENCE*ITAM OF SB RAS
Organization address
address: INSTITUTSKAYA 4/1 contact info |
RU (NOVOSIBIRSK) | participant | 28˙875.00 |
Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.
'The main objective of the study is the experimental and numerical study of gas surface interaction phenomena in the high enthalpy flow field behind the bow shock in front of a model at Martian entry flow conditions. The improvement of physical modelling using experimental data and its implementation into the CFD codes is essential to understand and interpret the physical processes. At the end the project will allow to estimate the aerothermal loads on the vehicle more accurately. Main activities of the project are: -Definition of requirements on experiments, modelling and CFD codes using realistic Mars mission profiles -Experiments on the measurement of flow parameters in the free stream and behind the shock and stagnation point heat flux rate -Improvement of existing physical models with respect to the non-equilibrium effects, transport properties and gas surface interaction chemistry -Implementation of improved physical models into the CFD codes and simulation of experiments -Synthesis of the data and extrapolation to the flight'