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ADEO: the European commercial passive de-orbit subsystem family enabling space debris mitigation

Stelzl, Daniel and Pfeiffer, Ernst K and Hemme, Hugo Garcia and Lindenmaier, Peter and Riemer, Arne and Cubillo, Alba Alegre and Spröwitz, Tom and Seefeldt, Patric and Meyer, Sebastian and Zander, Martin E. (2021) ADEO: the European commercial passive de-orbit subsystem family enabling space debris mitigation. CEAS Space Journal, 13, pp. 591-598. Springer. doi: 10.1007/s12567-021-00355-7. ISSN 1868-2502.

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Official URL: https://link.springer.com/article/10.1007/s12567-021-00355-7#citeas

Abstract

The ADEO subsystem is a scalable drag augmentation device that uses the residual Earth atmosphere present in Low Earth Orbit (LEO) to passively de-orbit of satellites between 1 and 2000 kg. For the de-orbit maneuvre, a large surface is deployed which multiplies the drag effective surface of the satellite significantly. Thereby the drag force is increased as well causing accelerated decay in orbit altitude. Advantageous about a drag augmentation device is that it does not require any active steering and can be designed for passive attitude stabilization thereby making it applicable for non-operational, tumbling spacecrafts as well. The ADEO subsystem consists of four deployable booms that span four sail segments in a planar shaped configuration. While the sails are made of an aluminum-coated polyimide foil, its coating thickness was chosen such that it provides sufficient protection from the LEO space environment. The current activity commenced in August 2018 is going to provide a fully qualified Protoflight Model (PFM) for a follow-up "In Orbit Demonstration" (IOD) in 2021/2022 (ADEO is selected as payload on the European Commission IOD/IOV satellite programme). In May 2020, the team passed the Manufacturing Readiness Review (MRR). An extensive Breadboarding- and Engineering Model campaign including life tests had already been carried out in 2019. The first ADEO-L PFM consists of a 5 m x 5 m dragsail deployed under control of own onboard electronics. Optionally, ADEO-L systems can be equipped with a so-called "watchdog routine" inside the electronics which is able to recognize the point in time when the satellite has come to the end of its life circle. With the help of an on-board battery the sail will be deployed automatically after a certain time in orbit. Operating like this, ADEO-L can be truly called "100% passive", a "CleanGreen Space Mission". First commercial candidate missions to be targeted after the successful EC-IOD mission were already identified by Airbus DS (DE) and QinetiQ (BE).

Item URL in elib:https://elib.dlr.de/146827/
Document Type:Article
Title:ADEO: the European commercial passive de-orbit subsystem family enabling space debris mitigation
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Stelzl, DanielHTS GmbHUNSPECIFIEDUNSPECIFIED
Pfeiffer, Ernst KHTS GmbHUNSPECIFIEDUNSPECIFIED
Hemme, Hugo GarciaHTS GmbHUNSPECIFIEDUNSPECIFIED
Lindenmaier, PeterHTS GmbHUNSPECIFIEDUNSPECIFIED
Riemer, ArneHTS GmbHUNSPECIFIEDUNSPECIFIED
Cubillo, Alba AlegreRuag Space Germany GmbHUNSPECIFIEDUNSPECIFIED
Spröwitz, TomUNSPECIFIEDhttps://orcid.org/0000-0001-5369-6919UNSPECIFIED
Seefeldt, PatricUNSPECIFIEDhttps://orcid.org/0000-0002-2067-9458UNSPECIFIED
Meyer, SebastianUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Zander, Martin E.UNSPECIFIEDhttps://orcid.org/0000-0001-5972-2938UNSPECIFIED
Date:24 March 2021
Journal or Publication Title:CEAS Space Journal
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:13
DOI:10.1007/s12567-021-00355-7
Page Range:pp. 591-598
Publisher:Springer
ISSN:1868-2502
Status:Published
Keywords:Passive De-orbit CleanGreen Space Mission Dragsail Cleanspace Space Debris Mitigation Reference Mission Proto Flight Model
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space System Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Space System Technology
DLR - Research theme (Project):R - GoSolAr (Gossamer Solar Array), R - Ultralight Photovoltaic Arrays
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Mechanic and Thermal Systems
Institute of Composite Structures and Adaptive Systems > Functional Lightweight Structures
Deposited By: Seefeldt, Patric
Deposited On:06 Dec 2021 14:35
Last Modified:06 Dec 2021 14:35

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