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Recovery and Return-To-Base European Reusable Micro-Launcher Project

Project description

RRTB - A disruptive recovery system for small rockets

The demand for small satellites (with masses lower than 500 kg) is being fuelled by numerous industries, from agriculture and energy, to civil engineering and defence. To serve this market, microlaunchers are being developed all over the world. However, in order to offer cost-effective and flexible access to space for small satellites, technological and operational innovation is fundamental. The EU-funded RRTB project will develop a disruptive recovery system that will allow the reuse of the first stage of the MESO microlauncher. The project studies the atmospheric re-entry of the vehicle, the landing phase of the first stage using novel electric ducted fans and the design of robust and reusable structure and cryogenic tanks.

Objective

The rise of small satellites and large constellations is changing the satellite industry. Due to the growth of the small satellite market, launch has become the bottleneck of the industry. According to MT Aerospace the micro-launcher market will grow as much as four to seven times in the next decade, with a full market potential of up to €7B.

The RRTB consortium believes that a tailored service for access to space for small satellites is required. However, micro-launchers regularly have higher launch costs per kilogram than bigger launchers. Today, the cornerstone of this emerging market is the economic viability of launching small payloads at high frequencies to dedicated orbits. According to the RRTB consortium, technological development and vehicle reuse are fundamental steps to bring down the cost of launch and access-to-space.

This project investigates the recovery and return to base system (RRTB) for the first stage of the MESO launch vehicle. The recovery and return to base system is divided into two parts:
1. Passive atmospheric reentry: The atmospheric reentry of the first stage of the vehicle will be a passive reentry. During the project this phase, together with its required hardware, will be investigated and defined during the project by Pangea Aerospace together with Deimos Space and VKI.
2. Horizontal landing: Landing of the first stage of the vehicle is intended to be performed using a novel patent pending horizontal landing technology that uses electric ducted fans situated in both sides of the first stage of the launch vehicle to brake the fall of first stage, control it and perform a safe landing. This phase will be studied by TUM and Pangea Aerospace.

Furthermore during the project the structural design and analysis of the MESO launch vehicle, as well as an investigation of the launch vehicle's propellant tanks (a critical component for cost-efficient reuse), will be performed. This work will involve RWTH, Heron, TAS, Toseda and Pangea.

Fields of science (EuroSciVoc)

Keywords

Programme(s)

Topic(s)

Funding Scheme

RIA - Research and Innovation action

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Call for proposal

(opens in new window) H2020-SPACE-2018-2020

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Coordinator

PANGEA AEROSPACE SL
Net EU contribution
€ 365 750,00
Address
AVENIDA NUMERO 1 NUM 20 PLANTA 1 EDIF B2.1
08040 Barcelona
Spain
SME
Yes
Region
Este Cataluña Barcelona
Activity type
Private for-profit entities (excluding Higher or Secondary Education Establishments)
Links
Total cost
€ 365 750,00

Participants (7)