Advancing Space Access Capabilities - Reusability and Multiple Satellite Injection | ASCenSIon | Progetto | Risultati | H2020 | CORDIS

CORDIS fornisce collegamenti ai risultati finali pubblici e alle pubblicazioni dei progetti ORIZZONTE.

I link ai risultati e alle pubblicazioni dei progetti del 7° PQ, così come i link ad alcuni tipi di risultati specifici come dataset e software, sono recuperati dinamicamente da .OpenAIRE .

Risultati finali

Definition and design of a laboratory set-up for an electrical pump-feeding system
Description of the 1D modelling code for HRE complete system
Validated regression rate measurement technique for HRE
Database for retro engines with reverse-flow interactions
First Year Report (SOTA and Methodology)

D6.1 is a first year report according to the French model, including a CV of the ESR, a detailed presentation of the subject including the SOTA (bibliography), a description of the methodology to be implemented to tackle the IRP, a presentation of first obtained results (if applicable). Going beyond the current standard, the documents of all ESRs will be combined to one collective report for the whole project, representing the overall SOTA of launcher research. Furthermore, the report will be reviewed by the supervisory teams to ensure that the ESRs are on track.

Multiple payload delivery scenarios analysis, GNC methods and architecture selection
Algorithms for health monitoring of RLV
Multidisciplinary GNC verification, performances, sensitivity analysis results
Systematic architecture trade-offs for RLV
Reliability model for novel launcher concepts
Performance of green propellant prototypes
Derivation of favourable engine and nozzle layouts for retro propulsion applications
Requirements for upper stages utilising green propellants
First database of experimental HRE results
Upper stage design for lower orbit to GTO of reusable TSTO launchers
Assessment (performance & heat loads) of nozzle options including novel design solutions for main and upper stages
Plan for Exploitation and Dissemination of Results (PEDR)

Plan for Exploitation and Dissemination of Results (PEDR) - Version 1. The PEDR will be updated throughout the project.

Six Degree-Of-Freedom (DOF) re-entry dynamics model
Re-entry GNC methods & architecture definition and preliminary verification
Validation of nozzle design approach with experimental data
Performance & life time data of prototype electric pump feeding system for H2O2/Eth.
RLV design guidelines and engineering methods
Communication strategy report

Communication strategy report - the report will be updated throughout the project.

Requirements and models for green propellant engines

Fellow profile advertisement flyer

ASCenSIon Video
Website

Project Website

Special issue of Acta Astronautica
Textbook (Springer)
Final conference

Pubblicazioni

RLV applications: challenges and benefits of novel technologies for sustainable main stages

Autori: Mateusz T. Gulczyński, Andrea Vennitti, Giuseppe Scarlatella, Guillermo J. Dominguez Calabuig, Lily Blondel-Canepari, Felix Weber, Alberto Sarritzu, Christian Bach, Jan Deeken, Tino Schmiel, Daniele Bianchi, Angelo Pasini
Pubblicato in: 2021
Editore: International Astronautical Federation, IAF

Design of the Optimal Trajectory for Multi-Payload Multi-Orbit Injection for an Upper Stage

Autori: Alforja Ruiz, I.; Lavagna, M.
Pubblicato in: 9th European Conference for Aerospace Sciences (EUCASS 2022), 2022, 2022
Editore: EUCASS-CEAS

Investigation of additive manufacturing techniques for paraffin-based fuel grains

Autori: R. Gelain, A. Hauw, E. Bardotti, P. Hendrick
Pubblicato in: 2021
Editore: The Italian Association of Aeronautics and Astronautics

Assessment of Mission Capabilities of a Reusable Heavy-lift Launch Vehicle Concept with Aerospike Engine

Autori: Giuseppe Scarlatella; Jacopo Guadagnini; Leonardo Paniccià; Gabriele De Zaiacomo; Martin Tajmar; Christian Bach; Dario Pastrone
Pubblicato in: AIAA SCITECH 2024 Forum, 2024
Editore: Aerospace research Central (ARC)
DOI: 10.2514/6.2024-2122

Mission Analysis, GNC and ATD for Reusable Launch Vehicles within ASCenSIon: Multi-Orbit Multi-Payload Injection, Re-Entry and Safe Disposal

Autori: ALFORJA RUIZ, IÑIGO Ayala Fernández, L. De OLIVEIRA, ALICE MARIE ANASTASIA Dominguez Calabuig, G. J. GUADAGNINI, JACOPO Lantelme, M. Bartoli, N. Chedevergne, F. De Zaiacomo, G. Dubreuil, S. LAVAGNA, MICHÈLE ROBERTA Prevereaud, Y. Stoll, E
Pubblicato in: 2021
Editore: International Astronautical Federation, IAF

Entry Corridor Analysis for Vertical Landing Reusable Launch Vehicles

Autori: Guadagnini, J.; Bonetti, D.; De Zaiacomo, G.
Pubblicato in: 2021
Editore: The Italian Association of Aeronautics and Astronautics

Advanced Nozzle Concepts in retro-propulsion applications for Reusable Launch Vehicle recovery: a case study

Autori: Giuseppe Scarlatella, Prof. Martin Tajmar, Dr.-Ing. Christian Bach
Pubblicato in: 2021
Editore: International Astronautical Federation, IAF

Green propellants and electric pump feeding system: challenges and opportunities of using these technologies for future kick stages

Autori: L. Ordoñez Valles, L. Blondel Canepari, A. Pasini, U. Apel, M. Tajmar
Pubblicato in: 2021
Editore: the Italian Association of Aeronautics and Astronautics

Reusable Launch Vehicles Re-Entry: Preliminary Architecture Towards Optimal Guidance and Control

Autori: Alice De Oliveira, Michèle Lavagna
Pubblicato in: 2021
Editore: The Italian Association of Aeronautics and Astronautics

Expansion-Deflection Nozzle Design and Performance Optimization for Upper-Stage Applications

Autori: Weber Felix, Bianchi Daniele and Nasuti Francesco
Pubblicato in: 9th Edition of the 3AF International Conference on Space Propulsion, 2024
Editore: 3AF

Guidance, Navigation and Control System Design for Multi-Payload and Multi-Orbit Injection

Autori: Alforja Ruiz, I.; Lavagna, M.
Pubblicato in: 2021
Editore: The Italian Association of Aeronautics and Astronautics

Introduction to sensor investigation for rlv health monitoring system

Autori: Andrea Vennitti, Tino Schmiel, Christian Bach, Martin Tajmar
Pubblicato in: 2021
Editore: The Italian Association of Aeronautics and Astronautics

Sensitivity Analysis of Propulsion System Parameters on GNC Strategies for Multi-Orbit Deliveries

Autori: Alforja Ruiz, I.; Blondel-Canepari, L.; Sarritzu, A.; Pasini, A.; Lavagna, M.
Pubblicato in: Aerospace Europe Conference 2023 - Joint 10th EUCASS - 9th CEAS Conference, 2023, 2023
Editore: EUCASS-CEAS

Analysis of Space Launch Vehicle Failures

Autori: Lucía Ayala Fernández, Carsten Wiedemann, Vitali Braun
Pubblicato in: 2021
Editore: The Italian Association of Aeronautics and Astronautics
DOI: 10.24355/dbbs.084-202202091543-0

Optical investigation of paraffin-based fuel combustion in a hybrid rocket slab burner

Autori: Gelain, Riccardo; De Morais Bertoldi, Artur Elias; Hendrick, Patrick; Lefebvre, Michel
Pubblicato in: Aerospace Europe Conference 2023, 2023
Editore: 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS

Advanced nozzle concept trade-off and selection criteria based on launcher mission constraints

Autori: Weber Felix, Bianchi Daniele and Nasuti Francesco
Pubblicato in: 9th European Conference for Aeronautics and Space Sciences, 2022
Editore: EUCASS-CEAS
DOI: 10.13009/eucass2022-4855

Comparison between a 400N Electric Pump Fed Hydrogen Peroxide/Ethanol Thruster and the MMH/NTO Legacy Systems

Autori: Livia Ordonez Valles, Uwe Apel, Martin Tajmar, Peter Weuta
Pubblicato in: 2021
Editore: International Astronautical Federation, IAF

Analyzing the potentialities of an electric pump-fed new generation kick stage powered by green propellants: a sensitivity analysis approach

Autori: Livia Ordonez Valles, Uwe Apel, Angelo Pasini, Martin Tajmar
Pubblicato in: SciTech 2023, 2023
Editore: SciTech

Review of regression rate enhancement techniques for hybrid rocket engines

Autori: Christopher Glaser, Jouke Hijlkema, Jérôme Anthoine
Pubblicato in: 2021
Editore: The Italian Association of Aeronautics and Astronautics

Cold-Gas Experiments on Advanced Nozzles in Subsonic Counter-Flows

Autori: Giuseppe Scarlatella; Theodor Heutling; Jan Sieder-Katzmann; Felix Weber; Marco Portolani; Marco Garutti; Daniele Bianchi; Andrea Ferrero; Dario G Pastrone; Martin Tajmar; Christian Bach
Pubblicato in: Aerospace Europe Conference 2023, 2023
Editore: 10th EUCASS - 9th CEAS

Conceptual study of technologies enabling novel green expendable upper stages with multi-payload/multi-orbit injection capability

Autori: Blondel-Canepari, Lily; Alforja Ruiz, Iñigo; Ayala Fernández, Lucía; Gelain, Riccardo; Glaser, Christopher; Ordoñez Valles, Livia; Sarritzu, Alberto; Anthoine, Jerôme; Apel, Uwe; Hendrick, Patrick; Hijlkema, Jouke; Lavagna, Michèle; Stoll, Enrico; Tajmar, Martin; Pasini, Angelo
Pubblicato in: 2021
Editore: The Italian Association of Aeronautics and Astronautics

Semantic Image Segmentation of Hybrid Rocket Fuel Combustion Data using Convolutional Neural Networks

Autori: Assenmacher, Oliver; Rüttgers, Alexander; Petrarolo, Anna; Gelain, Riccardo
Pubblicato in: AIAA SCITECH 2024 Forum, 2024
Editore: Aerospace Research Central (ARC)
DOI: 10.2514/6.2024-0799

COLD-FLOW TESTS ON ADVANCED NOZZLE CONCEPTS IN SUBSONIC RETRO-FLOWS: DEVELOPMENT OF TEST-BENCH

Autori: Giuseppe Scarlatella, Jan Sieder-Katzmann, Florian Roßberg, Felix Weber, Prof. Martin Tajmar, Dr.-Ing. Christian Bach
Pubblicato in: 2021
Editore: The Italian Association of Aeronautics and Astronautics

Numerical study of advanced nozzles for retro-propulsion applications and comparison with experimental data

Autori: Giuseppe Scarlatella
Pubblicato in: ASCenSIon Conference, 2023
Editore: ASCenSIon

Bridging the Technology Gap: Strategies for Hybrid Rocket Engines

Autori: C. Glaser, J. Hijlkema, J. Anthoine
Pubblicato in: Aerospace Journal, 2023, ISSN 2226-4310
Editore: MDPI
DOI: 10.3390/aerospace10100901

È in corso la ricerca di dati su OpenAIRE...

Advancing Space Access Capabilities - Reusability and Multiple Satellite Injection

Risultati finali

Pubblicazioni

Condividi questa pagina Condividi questa pagina sui social network

Scarica Scarica il contenuto della pagina