ERD

Wind Tunnel Experiments of Interstage Segments used for Aerodynamic Control of Retro-Propulsion Assisted Landing Vehicle...

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Retro Propulsion Assisted Landing Technologies (RETALT): Current Status and Outlook of the EU funded project on Reusable...

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Fin actuation, thrust vector control and landing leg mechanisms design for the RETALT VTVL launcher

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Design and Manufacturing Status of Advanced Structures for Reusable Launch Systems Demonstrators with Retro Propulsion A...

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Design and Manufacturing Status of Advanced Structures for Reusable Launch Systems Demonstrators with Retro Propulsion A...

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Retro propulsion assisted landing technologies: the RETALT project

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

RETALT - RETro propulsion Assisted Landing Technologies

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Periodic Reporting for period 2 - RETALT (Retro Propulsion Assisted Landing Technologies)

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Design of the Return GNC solution for the Retro-Propulsive Vertical Landing of RETALT

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Aerothermal databases and load predictions for Retro Propulsion-Assisted Launch Vehicles (RETALT)

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Optimum GNC Solutions for the Recovery and Vertical Landing of an Orbital Launch Vehicle

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

RETALT: Development of an Optimal GNC Solution for Recovery of an Orbital Launch Vehicle

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Landing Leg and Aerodynamic Control Surface Mechanisms and Functional Demonstrators for the RETALT1 Launch Vehicle

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Drop Test Description and Evaluation of a Landing Leg for a Re-usable Future Launche Vehicle

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Dissemination and Exploitation Report (all Partners)

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Dissemination and Exploitation Plan (all Partners)

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Mission Requirements Catalogue (DLR)

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Financial Report (all Partners)

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Press Release, project logo, templates for presentations and reports (CFSE)

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

FQ, Stability and Controllability Summary Report (DEIMOS)

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

RETALT: Recovery GNC for the Retro-Propulsive Vertical Landing of an Orbital Launch Vehicle

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

RETALT: Development of Key Flight Dynamics and GNC Technologies for Reusable Launchers

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

RETALT: review of technologies and overview of design changes

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Mission Engineering for the RETALT VTVL launcher

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Aerodynamic Phenomena of Retro Propulsion Descent and Landing Configurations

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Computational fluid dynamics investigations of aerodynamic control surfaces of a vertical landing configuration

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Key Technologies for Retro Propulsive Vertical Descent and Landing – RETALT – An Overview

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Hypersonic retro propulsion for reusable launch vehicles tested in the H2K wind tunnel

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Aerodynamic investigations of a Vertical Landing Launcher configuration by means of Computational Fluid Dynamics and Win...

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

TPS Design and Manufacturing for the RETALT VTVL launcher

Project: RETALT

Updated at: 29-04-2024

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Project acronym RETALT

Resources

Selected filters:

Wind Tunnel Experiments of Interstage Segments used for Aerodynamic Control of Retro-Propulsion Assisted Landing Vehicle...

Retro Propulsion Assisted Landing Technologies (RETALT): Current Status and Outlook of the EU funded project on Reusable...

Fin actuation, thrust vector control and landing leg mechanisms design for the RETALT VTVL launcher

Design and Manufacturing Status of Advanced Structures for Reusable Launch Systems Demonstrators with Retro Propulsion A...

Design and Manufacturing Status of Advanced Structures for Reusable Launch Systems Demonstrators with Retro Propulsion A...

Retro propulsion assisted landing technologies: the RETALT project

RETALT - RETro propulsion Assisted Landing Technologies

Periodic Reporting for period 2 - RETALT (Retro Propulsion Assisted Landing Technologies)

Design of the Return GNC solution for the Retro-Propulsive Vertical Landing of RETALT

Aerothermal databases and load predictions for Retro Propulsion-Assisted Launch Vehicles (RETALT)

Optimum GNC Solutions for the Recovery and Vertical Landing of an Orbital Launch Vehicle

RETALT: Development of an Optimal GNC Solution for Recovery of an Orbital Launch Vehicle

Landing Leg and Aerodynamic Control Surface Mechanisms and Functional Demonstrators for the RETALT1 Launch Vehicle

Drop Test Description and Evaluation of a Landing Leg for a Re-usable Future Launche Vehicle

Dissemination and Exploitation Report (all Partners)

Dissemination and Exploitation Plan (all Partners)

Mission Requirements Catalogue (DLR)

Financial Report (all Partners)

Press Release, project logo, templates for presentations and reports (CFSE)

FQ, Stability and Controllability Summary Report (DEIMOS)

RETALT: Recovery GNC for the Retro-Propulsive Vertical Landing of an Orbital Launch Vehicle

RETALT: Development of Key Flight Dynamics and GNC Technologies for Reusable Launchers

RETALT: review of technologies and overview of design changes

Mission Engineering for the RETALT VTVL launcher

Aerodynamic Phenomena of Retro Propulsion Descent and Landing Configurations

Computational fluid dynamics investigations of aerodynamic control surfaces of a vertical landing configuration

Key Technologies for Retro Propulsive Vertical Descent and Landing – RETALT – An Overview

Hypersonic retro propulsion for reusable launch vehicles tested in the H2K wind tunnel

Aerodynamic investigations of a Vertical Landing Launcher configuration by means of Computational Fluid Dynamics and Win...

TPS Design and Manufacturing for the RETALT VTVL launcher