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

Resultado final

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

Publicaciones

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

Autores: 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
Publicado en: 2021
Editor: International Astronautical Federation, IAF

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

Autores: Alforja Ruiz, I.; Lavagna, M.
Publicado en: 9th European Conference for Aerospace Sciences (EUCASS 2022), 2022, 2022
Editor: EUCASS-CEAS

Investigation of additive manufacturing techniques for paraffin-based fuel grains

Autores: R. Gelain, A. Hauw, E. Bardotti, P. Hendrick
Publicado en: 2021
Editor: The Italian Association of Aeronautics and Astronautics

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

Autores: 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
Publicado en: 2021
Editor: International Astronautical Federation, IAF

Entry Corridor Analysis for Vertical Landing Reusable Launch Vehicles

Autores: Guadagnini, J.; Bonetti, D.; De Zaiacomo, G.
Publicado en: 2021
Editor: The Italian Association of Aeronautics and Astronautics

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

Autores: Giuseppe Scarlatella, Prof. Martin Tajmar, Dr.-Ing. Christian Bach
Publicado en: 2021
Editor: International Astronautical Federation, IAF

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

Autores: L. Ordoñez Valles, L. Blondel Canepari, A. Pasini, U. Apel, M. Tajmar
Publicado en: 2021
Editor: the Italian Association of Aeronautics and Astronautics

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

Autores: Alice De Oliveira, Michèle Lavagna
Publicado en: 2021
Editor: The Italian Association of Aeronautics and Astronautics

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

Autores: Weber Felix, Bianchi Daniele and Nasuti Francesco
Publicado en: 9th Edition of the 3AF International Conference on Space Propulsion, 2024
Editor: 3AF

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

Autores: Alforja Ruiz, I.; Lavagna, M.
Publicado en: 2021
Editor: The Italian Association of Aeronautics and Astronautics

Introduction to sensor investigation for rlv health monitoring system

Autores: Andrea Vennitti, Tino Schmiel, Christian Bach, Martin Tajmar
Publicado en: 2021
Editor: The Italian Association of Aeronautics and Astronautics

Analysis of Space Launch Vehicle Failures

Autores: Lucía Ayala Fernández, Carsten Wiedemann, Vitali Braun
Publicado en: 2021
Editor: The Italian Association of Aeronautics and Astronautics
DOI: 10.24355/dbbs.084-202202091543-0

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

Autores: Weber Felix, Bianchi Daniele and Nasuti Francesco
Publicado en: 9th European Conference for Aeronautics and Space Sciences, 2022
Editor: EUCASS-CEAS
DOI: 10.13009/eucass2022-4855

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

Autores: Livia Ordonez Valles, Uwe Apel, Martin Tajmar, Peter Weuta
Publicado en: 2021
Editor: International Astronautical Federation, IAF

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

Autores: Livia Ordonez Valles, Uwe Apel, Angelo Pasini, Martin Tajmar
Publicado en: SciTech 2023, 2023
Editor: SciTech

Review of regression rate enhancement techniques for hybrid rocket engines

Autores: Christopher Glaser, Jouke Hijlkema, Jérôme Anthoine
Publicado en: 2021
Editor: The Italian Association of Aeronautics and Astronautics

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

Autores: 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
Publicado en: 2021
Editor: The Italian Association of Aeronautics and Astronautics

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

Autores: Giuseppe Scarlatella, Jan Sieder-Katzmann, Florian Roßberg, Felix Weber, Prof. Martin Tajmar, Dr.-Ing. Christian Bach
Publicado en: 2021
Editor: The Italian Association of Aeronautics and Astronautics

Buscando datos de OpenAIRE...

Advancing Space Access Capabilities - Reusability and Multiple Satellite Injection

Resultado final

Publicaciones

Compartir esta página

Descargar