Advancing Space Access Capabilities - Reusability and Multiple Satellite Injection

Informations projet

ASCenSIon

N° de convention de subvention: 860956

DOI 10.3030/860956

Projet clôturé

Date de signature de la CE 19 Août 2019

Date de début 1 Janvier 2020

Date de fin 29 Février 2024

Financé au titre de

• EXCELLENT SCIENCE - Marie Skłodowska-Curie Actions

Coût total € 3 881 057,76

Contribution de l’UE € 3 881 057,76

Coordonné par

TECHNISCHE UNIVERSITAET DRESDEN
Germany

Livrables

Other (1)

Fellow profile advertisement flyer

Websites, patent fillings, videos etc. (1)

Website

Project Website

Documents, reports (2)

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.

Communication strategy report

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

Publications

Conference proceedings (15)

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

Auteurs: 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
Publié dans: 2021
Éditeur: International Astronautical Federation, IAF

Investigation of additive manufacturing techniques for paraffin-based fuel grains

Auteurs: R. Gelain, A. Hauw, E. Bardotti, P. Hendrick
Publié dans: 2021
Éditeur: 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

Auteurs: 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
Publié dans: 2021
Éditeur: International Astronautical Federation, IAF

Entry Corridor Analysis for Vertical Landing Reusable Launch Vehicles

Auteurs: Guadagnini, J.; Bonetti, D.; De Zaiacomo, G.
Publié dans: 2021
Éditeur: The Italian Association of Aeronautics and Astronautics

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

Auteurs: Giuseppe Scarlatella, Prof. Martin Tajmar, Dr.-Ing. Christian Bach
Publié dans: 2021
Éditeur: International Astronautical Federation, IAF

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

Auteurs: L. Ordoñez Valles, L. Blondel Canepari, A. Pasini, U. Apel, M. Tajmar
Publié dans: 2021
Éditeur: the Italian Association of Aeronautics and Astronautics

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

Auteurs: Alice De Oliveira, Michèle Lavagna
Publié dans: 2021
Éditeur: The Italian Association of Aeronautics and Astronautics

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

Auteurs: Alforja Ruiz, I.; Lavagna, M.
Publié dans: 2021
Éditeur: The Italian Association of Aeronautics and Astronautics

Introduction to sensor investigation for rlv health monitoring system

Auteurs: Andrea Vennitti, Tino Schmiel, Christian Bach, Martin Tajmar
Publié dans: 2021
Éditeur: The Italian Association of Aeronautics and Astronautics

Analysis of Space Launch Vehicle Failures

Auteurs: Lucía Ayala Fernández, Carsten Wiedemann, Vitali Braun
Publié dans: 2021
Éditeur: The Italian Association of Aeronautics and Astronautics
DOI: 10.24355/dbbs.084-202202091543-0

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

Auteurs: Livia Ordonez Valles, Uwe Apel, Martin Tajmar, Peter Weuta
Publié dans: 2021
Éditeur: International Astronautical Federation, IAF

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

Auteurs: Livia Ordonez Valles, Uwe Apel, Angelo Pasini, Martin Tajmar
Publié dans: SciTech 2023, 2023
Éditeur: SciTech

Review of regression rate enhancement techniques for hybrid rocket engines

Auteurs: Christopher Glaser, Jouke Hijlkema, Jérôme Anthoine
Publié dans: 2021
Éditeur: The Italian Association of Aeronautics and Astronautics

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

Auteurs: 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
Publié dans: 2021
Éditeur: The Italian Association of Aeronautics and Astronautics

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

Auteurs: Giuseppe Scarlatella, Jan Sieder-Katzmann, Florian Roßberg, Felix Weber, Prof. Martin Tajmar, Dr.-Ing. Christian Bach
Publié dans: 2021
Éditeur: The Italian Association of Aeronautics and Astronautics