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

Leistungen

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

Veröffentlichungen

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

Autoren: 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
Veröffentlicht in: 2021
Herausgeber: International Astronautical Federation, IAF

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

Autoren: Alforja Ruiz, I.; Lavagna, M.
Veröffentlicht in: 9th European Conference for Aerospace Sciences (EUCASS 2022), 2022, 2022
Herausgeber: EUCASS-CEAS

Investigation of additive manufacturing techniques for paraffin-based fuel grains

Autoren: R. Gelain, A. Hauw, E. Bardotti, P. Hendrick
Veröffentlicht in: 2021
Herausgeber: 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

Autoren: 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
Veröffentlicht in: 2021
Herausgeber: International Astronautical Federation, IAF

Entry Corridor Analysis for Vertical Landing Reusable Launch Vehicles

Autoren: Guadagnini, J.; Bonetti, D.; De Zaiacomo, G.
Veröffentlicht in: 2021
Herausgeber: The Italian Association of Aeronautics and Astronautics

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

Autoren: Giuseppe Scarlatella, Prof. Martin Tajmar, Dr.-Ing. Christian Bach
Veröffentlicht in: 2021
Herausgeber: International Astronautical Federation, IAF

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

Autoren: L. Ordoñez Valles, L. Blondel Canepari, A. Pasini, U. Apel, M. Tajmar
Veröffentlicht in: 2021
Herausgeber: the Italian Association of Aeronautics and Astronautics

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

Autoren: Alice De Oliveira, Michèle Lavagna
Veröffentlicht in: 2021
Herausgeber: The Italian Association of Aeronautics and Astronautics

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

Autoren: Weber Felix, Bianchi Daniele and Nasuti Francesco
Veröffentlicht in: 9th Edition of the 3AF International Conference on Space Propulsion, 2024
Herausgeber: 3AF

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

Autoren: Alforja Ruiz, I.; Lavagna, M.
Veröffentlicht in: 2021
Herausgeber: The Italian Association of Aeronautics and Astronautics

Introduction to sensor investigation for rlv health monitoring system

Autoren: Andrea Vennitti, Tino Schmiel, Christian Bach, Martin Tajmar
Veröffentlicht in: 2021
Herausgeber: The Italian Association of Aeronautics and Astronautics

Analysis of Space Launch Vehicle Failures

Autoren: Lucía Ayala Fernández, Carsten Wiedemann, Vitali Braun
Veröffentlicht in: 2021
Herausgeber: 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

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

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

Autoren: Livia Ordonez Valles, Uwe Apel, Martin Tajmar, Peter Weuta
Veröffentlicht in: 2021
Herausgeber: International Astronautical Federation, IAF

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

Autoren: Livia Ordonez Valles, Uwe Apel, Angelo Pasini, Martin Tajmar
Veröffentlicht in: SciTech 2023, 2023
Herausgeber: SciTech

Review of regression rate enhancement techniques for hybrid rocket engines

Autoren: Christopher Glaser, Jouke Hijlkema, Jérôme Anthoine
Veröffentlicht in: 2021
Herausgeber: The Italian Association of Aeronautics and Astronautics

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

Autoren: 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
Veröffentlicht in: 2021
Herausgeber: The Italian Association of Aeronautics and Astronautics

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

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

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Advancing Space Access Capabilities - Reusability and Multiple Satellite Injection

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