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ASCenSIon SIGNED

Advancing Space Access Capabilities - Reusability and Multiple Satellite Injection

Total Cost €

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EC-Contrib. €

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Partnership

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 ASCenSIon project word cloud

Explore the words cloud of the ASCenSIon project. It provides you a very rough idea of what is the project "ASCenSIon" about.

interactions    ecological    engines    pump    payloads    disposal    electric    examination    propellants    flow    espss    training    layout    ascension    solutions    sites    networks    missionisation    extensive    hot    mission    prove    experimental    techniques    mitigation    reusable    edge    entry    safe    trajectory    critical    orbits    recovery    landing    constellations    rocket    feeding    integration    hybrid    utilisation    ecosimpro    navigation    simulations    purpose    strategies    insertion    multiple    demands    variety    aero    injecting    payload    debris    technologies    orbital    models    economical    runs    monitoring    numerical    descend    green    launcher    nozzle    subsystems    propulsion    cold    flexibility    feasibility    space    efficient    gnc    re    fire    reusability    sustainability    configurations    cover    dynamics    cutting    trajectories    reuse    stage    demand    health    durability    guidance    network    sensor    thermo    wireless    computational   

Project "ASCenSIon" data sheet

The following table provides information about the project.

Coordinator
TECHNISCHE UNIVERSITAET DRESDEN 

Organization address
address: HELMHOLTZSTRASSE 10
city: DRESDEN
postcode: 1069
website: http://www.tu-dresden.de/

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.

 Coordinator Country Germany [DE]
 Total cost 3˙881˙057 €
 EC max contribution 3˙881˙057 € (100%)
 Programme 1. H2020-EU.1.3.1. (Fostering new skills by means of excellent initial training of researchers)
 Code Call H2020-MSCA-ITN-2019
 Funding Scheme MSCA-ITN-ETN
 Starting year 2020
 Duration (year-month-day) from 2020-01-01   to  2023-12-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    TECHNISCHE UNIVERSITAET DRESDEN DE (DRESDEN) coordinator 505˙576.00
2    OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES FR (PALAISEAU) participant 549˙604.00
3    POLITECNICO DI MILANO IT (MILANO) participant 522˙999.00
4    DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV DE (KOELN) participant 505˙576.00
5    SITAEL SPA IT (MOLA DI BARI) participant 261˙499.00
6    UNIVERSITA DEGLI STUDI DI ROMA LA SAPIENZA IT (ROMA) participant 261˙499.00
7    UNIVERSITA DI PISA IT (PISA) participant 261˙499.00
8    UNIVERSITE LIBRE DE BRUXELLES BE (BRUXELLES) participant 256˙320.00
9    HOCHSCHULE BREMEN DE (Bremen) participant 252˙788.00
10    TECHNISCHE UNIVERSITAET BRAUNSCHWEIG DE (BRAUNSCHWEIG) participant 252˙788.00
11    DEIMOS SPACE SOCIEDAD LIMITADA UNIPERSONAL ES (TRES CANTOS (MADRID)) participant 250˙904.00

Map

 Project objective

The purpose of the ASCenSIon project is to develop a programme that focuses on several specific areas of cutting edge space access research, particularly on launcher systems that are (partially) reusable and capable of injecting multiple payloads into multiple orbits. More than providing design concepts, the network aims to identify and advance critical technologies to prove a feasibility of these concepts. Fields of research and training include propulsion technologies and their reusability; Guidance, Navigation and Control (GNC); aero-thermo-dynamics of re-entry and safe disposal. A variety of technologies will be advanced, including hybrid rocket engines, electric pump feeding and advanced nozzle configurations. Both computational and experimental (cold-flow and hot fire) techniques will ensure an efficient process and reliable results. The reuse of propulsion systems demands an assessment of their durability. It will be conducted by numerical simulations, system analysis with EcosimPro/ESPSS and experimental test runs. The development and integration of wireless sensor networks will allow health monitoring of these critical subsystems. Moreover, novel GNC strategies and processes have to be developed for the whole mission trajectory. This includes solutions for optimised flexibility w.r.t. the orbital insertion conditions as well as dedicated descend trajectories and GNC missionisation for re-entry. The models will cover various recovery concepts and the support of multiple landing sites. This requires an extensive examination of the aero-thermo-dynamics during re-entry as well as of the interactions between stage recovery and propulsion system layout. Ecological and economical sustainability will be addressed as new payload concepts including large constellations increase the demand for safe disposal and space debris mitigation to ensure an open access to space in the future. Furthermore, the utilisation of so called green propellants will be investigated.

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The information about "ASCENSION" are provided by the European Opendata Portal: CORDIS opendata.

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