Advancing Space Access Capabilities - Reusability and Multiple Satellite Injection | ASCenSIon | Project | Results | H2020 | CORDIS

CORDIS oferuje możliwość skorzystania z odnośników do publicznie dostępnych publikacji i rezultatów projektów realizowanych w ramach programów ramowych HORYZONT.

Odnośniki do rezultatów i publikacji związanych z poszczególnymi projektami 7PR, a także odnośniki do niektórych konkretnych kategorii wyników, takich jak zbiory danych i oprogramowanie, są dynamicznie pobierane z systemu OpenAIRE .

Rezultaty

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

Publikacje

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

Autorzy: 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
Opublikowane w: 2021
Wydawca: International Astronautical Federation, IAF

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

Autorzy: Alforja Ruiz, I.; Lavagna, M.
Opublikowane w: 9th European Conference for Aerospace Sciences (EUCASS 2022), 2022, 2022
Wydawca: EUCASS-CEAS

Investigation of additive manufacturing techniques for paraffin-based fuel grains

Autorzy: R. Gelain, A. Hauw, E. Bardotti, P. Hendrick
Opublikowane w: 2021
Wydawca: The Italian Association of Aeronautics and Astronautics

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

Autorzy: Giuseppe Scarlatella; Jacopo Guadagnini; Leonardo Paniccià; Gabriele De Zaiacomo; Martin Tajmar; Christian Bach; Dario Pastrone
Opublikowane w: AIAA SCITECH 2024 Forum, 2024
Wydawca: 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

Autorzy: 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
Opublikowane w: 2021
Wydawca: International Astronautical Federation, IAF

Entry Corridor Analysis for Vertical Landing Reusable Launch Vehicles

Autorzy: Guadagnini, J.; Bonetti, D.; De Zaiacomo, G.
Opublikowane w: 2021
Wydawca: The Italian Association of Aeronautics and Astronautics

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

Autorzy: Giuseppe Scarlatella, Prof. Martin Tajmar, Dr.-Ing. Christian Bach
Opublikowane w: 2021
Wydawca: International Astronautical Federation, IAF

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

Autorzy: L. Ordoñez Valles, L. Blondel Canepari, A. Pasini, U. Apel, M. Tajmar
Opublikowane w: 2021
Wydawca: the Italian Association of Aeronautics and Astronautics

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

Autorzy: Alice De Oliveira, Michèle Lavagna
Opublikowane w: 2021
Wydawca: The Italian Association of Aeronautics and Astronautics

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

Autorzy: Weber Felix, Bianchi Daniele and Nasuti Francesco
Opublikowane w: 9th Edition of the 3AF International Conference on Space Propulsion, 2024
Wydawca: 3AF

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

Autorzy: Alforja Ruiz, I.; Lavagna, M.
Opublikowane w: 2021
Wydawca: The Italian Association of Aeronautics and Astronautics

Introduction to sensor investigation for rlv health monitoring system

Autorzy: Andrea Vennitti, Tino Schmiel, Christian Bach, Martin Tajmar
Opublikowane w: 2021
Wydawca: The Italian Association of Aeronautics and Astronautics

Analysis of Space Launch Vehicle Failures

Autorzy: Lucía Ayala Fernández, Carsten Wiedemann, Vitali Braun
Opublikowane w: 2021
Wydawca: 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

Autorzy: Gelain, Riccardo; De Morais Bertoldi, Artur Elias; Hendrick, Patrick; Lefebvre, Michel
Opublikowane w: Aerospace Europe Conference 2023, 2023
Wydawca: 10ᵀᴴ EUCASS – 9ᵀᴴ CEAS

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

Autorzy: Weber Felix, Bianchi Daniele and Nasuti Francesco
Opublikowane w: 9th European Conference for Aeronautics and Space Sciences, 2022
Wydawca: EUCASS-CEAS
DOI: 10.13009/eucass2022-4855

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

Autorzy: Livia Ordonez Valles, Uwe Apel, Martin Tajmar, Peter Weuta
Opublikowane w: 2021
Wydawca: International Astronautical Federation, IAF

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

Autorzy: Livia Ordonez Valles, Uwe Apel, Angelo Pasini, Martin Tajmar
Opublikowane w: SciTech 2023, 2023
Wydawca: SciTech

Review of regression rate enhancement techniques for hybrid rocket engines

Autorzy: Christopher Glaser, Jouke Hijlkema, Jérôme Anthoine
Opublikowane w: 2021
Wydawca: The Italian Association of Aeronautics and Astronautics

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

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

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

Autorzy: 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
Opublikowane w: 2021
Wydawca: The Italian Association of Aeronautics and Astronautics

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

Autorzy: Assenmacher, Oliver; Rüttgers, Alexander; Petrarolo, Anna; Gelain, Riccardo
Opublikowane w: AIAA SCITECH 2024 Forum, 2024
Wydawca: 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

Autorzy: Giuseppe Scarlatella, Jan Sieder-Katzmann, Florian Roßberg, Felix Weber, Prof. Martin Tajmar, Dr.-Ing. Christian Bach
Opublikowane w: 2021
Wydawca: The Italian Association of Aeronautics and Astronautics

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

Autorzy: Giuseppe Scarlatella
Opublikowane w: ASCenSIon Conference, 2023
Wydawca: ASCenSIon

Bridging the Technology Gap: Strategies for Hybrid Rocket Engines

Autorzy: C. Glaser, J. Hijlkema, J. Anthoine
Opublikowane w: Aerospace Journal, 2023, ISSN 2226-4310
Wydawca: MDPI
DOI: 10.3390/aerospace10100901

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