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European Recovery System (ERS)

Hörschgen, Marcus and Pfeuffer, Horst and Janke, Thomas (2009) European Recovery System (ERS). 19th ESA Symposium on European Rocket and Balloon Programmes and Related Research, 07.-11. Juni 2009, Bad Reichenhall, Deutschland.

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Abstract

Up to the TEXUS-44 microgravity research mission, successfully launched in February 2008, the payloads of the TEXUS vehicles were exclusively equipped with the Magellan (former Bristol Aerospace Ltd.) ORSA recovery system, integrated into the ogive nose cone. With the intention to gain more independency from the North American market and the inherent procurement and ITAR regulations problems, the European Space Agency (ESA) has taken initiative to contract industry for the development and built-up of a new European Recovery System (ERS) in 2006. For the design, manufacturing and qualification task sharing, a cooperation of DLR Moraba and the Kayser-Threde GmbH has been initialized. The ERS is designed to recover payloads of up to 450 kg mass and 17 inch (438 mm) diameter by a two-stage subsonic parachute system. It features a separating ogive nose tip with a forward deploying recovery parachute. The assembly incorporates a 3:1 fineness ratio ogive which forward portion is ejected exo-atmospherically to permit subsequent parachute recovery system operation. The aft ogive houses the parachute system, autonomous redundant pyrotechnic ignition system, housekeeping electronics, TM interface, beacon system, camera system and pyrotechnic and electronic batteries. The parachute system activation is controlled by barometric switches on the descent trajectory at a nominal altitude of 15 kft (4.6 km) in the combination of an electronic timing activation unit (ignition unit). Together with the heat shield ejection the drogue parachute is deployed and the payload is mainly stabilized from flat spin and decelerated. After complete stabilization the drogue parachute is separated and extracts the main parachute out of the deployment bag. At fully opened main parachute the final sink rate is around 8 m/sec.

Item URL in elib:https://elib.dlr.de/83907/
Document Type:Conference or Workshop Item (Speech)
Title:European Recovery System (ERS)
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hörschgen, MarcusDLRUNSPECIFIED
Pfeuffer, HorstKayser-ThredeUNSPECIFIED
Janke, ThomasDLRUNSPECIFIED
Date:2009
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:ERS, TEXUS, MASER, Sounding Rocket, Recovery, Parachute System, Ignition Unit, VSB-30
Event Title:19th ESA Symposium on European Rocket and Balloon Programmes and Related Research
Event Location:Bad Reichenhall, Deutschland
Event Type:international Conference
Event Dates:07.-11. Juni 2009
Organizer:ESA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Technik für Raumfahrtsysteme
DLR - Research theme (Project):R - Vorhaben Mobile Raketenbasis (MORABA)
Location: Oberpfaffenhofen
Institutes and Institutions:Space Operations and Astronaut Training > Mobile Rocket Base
Deposited By: Hörschgen-Eggers, Marcus
Deposited On:23 Sep 2013 10:07
Last Modified:31 Jul 2019 19:42

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