DOCSLIB.ORG

ESA Operational Collision Avoidance UNOOSA – Promoting Space Sustainability 25Th February 2021

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
ESA Operational Collision Avoidance UNOOSA – Promoting Space Sustainability 25Th February 2021 ESA Operational Collision Avoidance UNOOSA – Promoting Space Sustainability 25th February 2021 Francesca Letizia ESA Space Debris Office ESA UNCLASSIFIED - Releasable to the Public 1 Collision avoidance service: why Statistics Local perspective on space Collisions with objects debris at larger than 1 cm have the potential of prematurely ending a mission Global perspective Collisions can significantly contribute to the Cosmos-Iridium collision evolution of the debris 3294 new objects environment Accidental break-ups caused by collisions covered by standards (ISO 24113) and guidelines (UN LTS B.4) 2 Collision avoidance service: the missions Sentinel 2A/B Institutional Cryosat-2 missions Sentinel 3A/B Third-party Cheops missions Proba 2 Sentinel 1A/B SAOCOM-1A/B Additional support to non-LEO missions Swarm B (Cluster, XMM, Integral) Swarm A, C and during LEOPs (MSG, Galileo, MetopC, Aelous Sentinel 6) 3 Our process at a glance DISCOS Space object weather Read more about our properties models process at SSA data CDMs Automated providers retrieval Trajectories & Propagation MiniCat CRASS CORAM manoeuvre data Flight Interface dynamics monitoring SCARF Trajectories & covariance data visualisation Flight control Debris team analysts 4 Data sharing – Operational products DISCOS Space B1.1 object weather properties models SSA data CDMs Automated providers retrieval Provide contact information (e.g. through space-track.org) B1.2 Regularly update own satellites’ information (orbit & manoeuvre plan) Adopt standard formats when exchanging information: Trajectories & Propagation• CDMs issuedMiniCat by SSA data providersCRASS CORAM manoeuvre data • OEMs for orbit information B2.3 • OPMs for manoeuvre data Flight Interface dynamics monitoring SCARF Trajectories & covariance data visualisation 5 Data sharing – information on objects DISCOS Space B1.5 object weather properties models SSA data CDMs Automated providers retrieval Data curation for objects in space Assess provided worldwide • normal users: web-based interface Trajectories & Propagation MiniCat CRASS CORAM manoeuvre data• operational users: API available Backbone for several analysis activities such as compliance monitoring Flight Interface dynamics monitoring SCARF Trajectories & covariance data visualisation 6 Conjunction assessment DISCOS Space object weather properties models SSA data CDMs Automated Pool of chaser Check for Collision risk providers retrieval orbits and conjunctions computation covariance not in CDMs Trajectories & Propagation MiniCat CRASS CORAM B4 manoeuvre data + (if needed) design of the Flight Interface avoidance dynamics monitoring manoeuvre SCARF Trajectories & covariance data visualisation 7 Conjunction assessment DISCOS Space object weather properties models SSA data CDMs Automated Pool of chaser Check for Collision risk providers retrieval orbits and conjunctions computation covariance not in CDMs Trajectories & Propagation MiniCat CRASS CORAM B4 manoeuvre data C2 + (if needed) design of the We makeFlight available tools Interface(DRAMA) avoidance anddynamics methodologies to analysemonitoring the collision risk and reduction manoeuvre SCARF strategies duringTrajectories the design & of a missioncovariance data visualisation 8 Alerts & manoeuvres Escalated events = alert to missions collision probability near pre-defined threshold & conjunction closer than 3 days Manoeuvre collision probability above pre-defined threshold & conjunction closer than ~ 1 day For a Sentinel-like mission: • 1 alert/month • 1 manoeuvre/3 months For each manoeuvre • Negligible fuel consumption • ~8 hours of data outage 9 Alerts & manoeuvres Escalated events = alert to missions C4 collision probability near pre-defined threshold & conjunction closer than 3 days Manoeuvre collision probability above pre-defined threshold & conjunction closer than ~ 1 day For a Sentinel-like mission: • 1 alert/month • 1 manoeuvre/3 months For each manoeuvre • Negligible fuel consumption • ~8 hours of data outage 10 Conjunction statistics Data for events with collision probability > 10-6 11 Conjunction statistics Data for events with collision probability > 10-6 Payload-related debris Satellites Rocket-related debris 12 Emerging trends: towards more automated systems Current approach Research directions & future approaches Assessment of historical conjunctions and model training Approaches for automated (and explainable) decisions Advanced manoeuvre design Coordination of operators and Flight control Debris catalogue providers team analysts 13 Emerging trends: towards more automated systems Current approach Research directions & future approaches Assessment of historical conjunctions and model training Approaches for automated Open competition in 2019(and explainable)for researchers decisions to test machine learning approaches D1 Distribution of anonymised operational CDMs to support research inAdvanced conjunction manoeuvre evaluation design Coordination of operators and Flight control Debris catalogue providers team analysts 14 Emerging trends: small satellites & trackability 15 Conclusions UN LTS Collision avoidance an operational reality for actors in space: B1 convergence of self-interest and long-term sustainability of operations as captured in the UN LTS Guidelines B2 ESA process based on standardised products, curated object data, automated workflow + contribution in tools and B4 knowledge dissemination The changes in the use of space call for C2 • Increased data quality and sharing • Improved coordination methods C4 • Increased automation Developments in collisions avoidance activities are an important D1 pillar in ESA Space Safety Programme 16 Produced by Follow @esaoperations for the latest graphics and podcasts on collision avoidance activity & sustainable operations realised in collaboration with UNOOSA 17 Dr. Francesca Letizia ESA/ESOC Space Debris Office (OPS-SD) Robert-Bosch-Str. 5, 64293 Darmstadt, Germany T +496151902079 [email protected] http://www.esa.int/debris 18.
Load more

Recommended publications
  • CZ-Space Day Intro
    16.7.2010 ESA TECHNOLOGY → PROGRAMMES AND STRATEGY Czech Space Technology Day - GSTP July 2010 CONTENTS • The European Space Agency -ESA • Space Technology • ESA’s Technology Programmes • Doing business with ESA • ESA’s Long Term Plan 2 1 16.7.2010 → THE EUROPEAN SPACE AGENCY PURPOSE OF ESA “To provide for and promote, for exclusively peaceful purposes, cooperation among European states in space research and technology and their space applications. ” - Article 2 of ESA Convention 4 2 16.7.2010 ESA FACTS AND FIGURES • Over 30 years of experience • 18 Member States • Five establishments, about 2000 staff • 3.7 billion Euro budget (2010) • Over 60 satellites designed, tested and operated in flight • 17 scientific satellites in operation • Five types of launcher developed • Over 190 launches 5 18 MEMBER STATES Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece, Ireland, Italy, Luxembourg, Norway, the Netherlands, Portugal, Spain, Sweden, Switzerland and the United Kingdom. Canada takes part in some programmes under a Cooperation Agreement. Hungary, Romania, Poland, Slovenia, and Estonia are European Cooperating States. Cyprus and Latvia have signed Cooperation Agreements with ESA. 6 3 16.7.2010 ACTIVITIES ESA is one of the few space agencies in the world to combine responsibility in nearly all areas of space activity. • Space science • Navigation • Human spaceflight • Telecommunications • Exploration • Technology • Earth observation • Operations • Launchers 7 ESA PROGRAMMES All Member States participate (on In addition,
    [Show full text]
  • ACT-RPR-SPS-1110 Sps Europe Paper
    62nd International Astronautical Congress, Cape Town, SA. Copyright ©2011 by the European Space Agency (ESA). Published by the IAF, with permission and released to the IAF to publish in all forms. IAC-11-C3.1.3 PROSPECTS FOR SPACE SOLAR POWER IN EUROPE Leopold Summerer European Space Agency, Advanced Concepts Team, The Netherlands, [email protected] Lionel Jacques European Space Agency, Advanced Concepts Team, The Netherlands, [email protected] In 2002, a phased, multi-year approach to space solar power has been published. Following this plan, several activities have matured the concept and technology further in the following years. Despite substantial advances in key technologies, space solar power remains still at the weak intersections between the space sector and the energy sector. In the 10 years since the development of the European SPS Programme Plan, both, the space and the energy sectors have undergone substantial changes and many key enabling technologies for space solar power have advanced significantly. The present paper attempts to take account of these changes in view to assess how they influence the prospect for space solar power work for Europe. Fresh Look Study as well as the work on a European I INTRODUCTION sail tower concept by Klimke and Seboldt [16], [17]. Based on these results, which re-confirmed the The concept of generating solar power in space and principal technical viability of space solar power transmitting it to Earth to contribute to terrestrial energy concepts, the focus of the first phase of the European systems has received period attention since P. Glaser SPS programme plan has been to enlarge the evaluation published the first engineering approach to it in 1968 scope of space solar power by including expertise from [1].
    [Show full text]
  • → Space for Europe European Space Agency
    number 153 | February 2013 bulletin → space for europe European Space Agency The European Space Agency was formed out of, and took over the rights and The ESA headquarters are in Paris. obligations of, the two earlier European space organisations – the European Space Research Organisation (ESRO) and the European Launcher Development The major establishments of ESA are: Organisation (ELDO). The Member States are Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece, Ireland, Italy, Luxembourg, the ESTEC, Noordwijk, Netherlands. Netherlands, Norway, Poland, Portugal, Romania, Spain, Sweden, Switzerland and the United Kingdom. Canada is a Cooperating State. ESOC, Darmstadt, Germany. In the words of its Convention: the purpose of the Agency shall be to provide for ESRIN, Frascati, Italy. and to promote, for exclusively peaceful purposes, cooperation among European States in space research and technology and their space applications, with a view ESAC, Madrid, Spain. to their being used for scientific purposes and for operational space applications systems: Chairman of the Council: D. Williams (to Dec 2012) → by elaborating and implementing a long-term European space policy, by recommending space objectives to the Member States, and by concerting the Director General: J.-J. Dordain policies of the Member States with respect to other national and international organisations and institutions; → by elaborating and implementing activities and programmes in the space field; → by coordinating the European space programme and national programmes, and by integrating the latter progressively and as completely as possible into the European space programme, in particular as regards the development of applications satellites; → by elaborating and implementing the industrial policy appropriate to its programme and by recommending a coherent industrial policy to the Member States.
    [Show full text]
  • The EXOD Search for Faint Transients in XMM-Newton Observations
    UvA-DARE (Digital Academic Repository) The EXOD search for faint transients in XMM-Newton observations Method and discovery of four extragalactic Type I X-ray bursters Pastor-Marazuela, I.; Webb, N.A.; Wojtowicz, D.T.; van Leeuwen, J. DOI 10.1051/0004-6361/201936869 Publication date 2020 Document Version Final published version Published in Astronomy & Astrophysics Link to publication Citation for published version (APA): Pastor-Marazuela, I., Webb, N. A., Wojtowicz, D. T., & van Leeuwen, J. (2020). The EXOD search for faint transients in XMM-Newton observations: Method and discovery of four extragalactic Type I X-ray bursters. Astronomy & Astrophysics, 640, [A124]. https://doi.org/10.1051/0004-6361/201936869 General rights It is not permitted to download or to forward/distribute the text or part of it without the consent of the author(s) and/or copyright holder(s), other than for strictly personal, individual use, unless the work is under an open content license (like Creative Commons). Disclaimer/Complaints regulations If you believe that digital publication of certain material infringes any of your rights or (privacy) interests, please let the Library know, stating your reasons. In case of a legitimate complaint, the Library will make the material inaccessible and/or remove it from the website. Please Ask the Library: https://uba.uva.nl/en/contact, or a letter to: Library of the University of Amsterdam, Secretariat, Singel 425, 1012 WP Amsterdam, The Netherlands. You will be contacted as soon as possible. UvA-DARE is a service provided by the library of the University of Amsterdam (https://dare.uva.nl) Download date:02 Oct 2021 A&A 640, A124 (2020) Astronomy https://doi.org/10.1051/0004-6361/201936869 & c ESO 2020 Astrophysics The EXOD search for faint transients in XMM-Newton observations: Method and discovery of four extragalactic Type I X-ray bursters I.
    [Show full text]
  • Sentinel-2 and Sentinel-3 Mission Overview and Status
    Sentinel-2 and Sentinel-3 Mission Overview and Status Craig Donlon – Sentinel-3 Mission Scientist and Ferran Gascon – Sentinel-2 QC manager and others @ESA IOCCG-21, Santa Monica, USA 1-3rd March 2016 Overview – What is Copernicus? – Sentinel-2 mission and status – Sentinel-3 mission and status Sentinel-3A OLCI first light Svalbard: 29 Feb 14:07:45-14:09:45 UTC Bands 4, 6 and 7 (of 21) at 490, 560, 620 nm Spain and Gibraltar 1 March 10:32:48-10:34:48 UTC California USA 29 Feb 17:44:54-17:46:54 UTC What is Copernicus? Space Component In-Situ Services A European Data Component response to global needs 6 What is Copernicus? – Space in Action for You! • A source of information for policymakers, industry, scientists, business and the public • A European response to global issues: • manage the environment; • understand and to mitigate the effects of climate change; • ensure civil security • A user-driven programme of services for environment and security • An integrated Earth Observation system (combining space-based and in-situ data with Earth System Models) Components & Competences Coordinators: Partners: Private Space Industries companies Component National Space Agencies Overall Programme EMCWF EMSA Mercator snd Ocean Coordination FRONTEX Service Services operators Component EUSC EEA JRC In-situ data are supporting the Space and Services Components Copernicus Funding Funding for Development Funding for Operational Phase until 2013 (c.e.c.): Phase as from 2014 (c.e.c.): ~€ 3.7 B (from ESA and € 4.3 B for the EU) whole programme (from EU)
    [Show full text]
  • Update on PROBA-2 TDM and ALPHASAT TDP8 Flight Data
    Update on PROBA-2 TDM and ALPHASAT TDP8 Flight Data Christian POIVEY, Gerard PLANES CONANGLA, Marco d’ALESSIO, Reno HARBOE-SORENSEN ESA ESTEC CNES ESA Radiation Effects Final Presentations Days March 9&10, 2015 OUTLINE 1. PROBA-2 TDM 2. Summary of PROBA-2 TDM SEE flight data on memories 3. ALPHASAT TDP8 4. Summary of ALPHASAT TDP8 SEE flight data on memories CNES ESA Radiation Effects Final Presentations Days March 9&10, 2015 PROBA-2 Launched on November 2, 2009 LEO orbit: 713-733 km, 98 degrees inclination PROBA-2 - TDM 1. TDM : Memories on board TDM/Proba II a. TID (RADFETs) Atmel AT68166 (4*AT60142) 2M x 8 b. Reference SEU monitor Alliance AS7C34096A-12TI 512K x 8 c. SEL experiment Semi. – SEL Samsung K6R4008V1D 512K x 8 – SEU ISSI IS61LV5128AL-12 512K x 8 d. Flash memory experiment. 2. Period analyzed ISSI IS62WV20488BLL 2M x8 a. March 2010-January 2015 Samsung K9FG08U0M 1G x 8 – (1769 days) CNES ESA Radiation Effects Final Presentations Days March 9&10, 2015 PROBA-2 TDM CNES ESA Radiation Effects Final Presentations Days March 9&10, 2015 SEL experiment, SEL Data SEL experiment in TDM/Proba-2 Tot SAA Alliance Semi. AS7C34096A-12TI 512K x 8 3 2 Samsung K6R4008V1D-TI10 512K x 8 8 4 ISSI IS61LV5128AL-12 512K x 8 357 293 ISSI IS62WV20488BLL 2M x8 12 5 CNES ESA Radiation Effects Final Presentations Days March 9&10, 2015 SEL experiment, SEL Data IS61LV5128AL Differential latchup rate (smoothed in blue) CNES ESA Radiation Effects Final Presentations Days March 9&10, 2015 SEL experiment, SEL Data Comparison with Calculated Rates SEL rate prediction was performed for the 4 SRAMs using OMERE under solar maximum conditions, a sensitive volume thickness of 1 micron and 10 mm of Aluminum shielding.
    [Show full text]
  • Cluster Keeping Algorithms for the Satellite Swarm Sensor Network Project
    5th Federated and Fractionated Satellite Systems Workshop November 2-3, 2017, ISAE SUPAERO – Toulouse, France Cluster Keeping Algorithms for the Satellite Swarm Sensor Network Project Eviatar Edlerman and Pini Gurfil Technion – Israel Institute of Technology, Haifa 32000, Israel [email protected]; [email protected] Abstract This paper develops cluster control algorithms for the Satellite Swarm Sensor Network (S3Net) project, whose main aim is to enable fractionation of space-based remote sensing, imaging, and observation satellites. A methodological development of orbit control algorithms is provided, supporting the various use cases of the mission. Emphasis is given on outlining the algorithms structure, information flow, and software implementation. The methodology presented herein enables operation of multiple satellites in coordination, to enable fractionation of space sensors and augmentation of data provided therefrom. 1. INTRODUCTION In the field of earth observation from space, modern approaches show a trend of moving away from the classical single satellite missions, where one satellite includes a complete set of sensors and instruments, towards fractionated and distributed sensor missions, where multiple satellites, possibly carrying different types of sensors, act in a formation or swarm. Such missions promise an increase of imaging quality, an increase of service quality and, in many cases, a decrease of deployment costs for satellites that can become smaller and less complex due to mission requirements. Need for incremental deployment can be caused by funding limitations or issues. Although a combination of funds from different interest groups is possible, it can be difficult to achieve. A higher degree of independence for service providers can be enabled through lower cost satellites that allow integration into satellite swarms.
    [Show full text]
  • → Space for Europe European Space Agency
    number 149 | February 2012 bulletin → space for europe European Space Agency The European Space Agency was formed out of, and took over the rights and The ESA headquarters are in Paris. obligations of, the two earlier European space organisations – the European Space Research Organisation (ESRO) and the European Launcher Development The major establishments of ESA are: Organisation (ELDO). The Member States are Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece, Ireland, Italy, Luxembourg, the ESTEC, Noordwijk, Netherlands. Netherlands, Norway, Portugal, Romania, Spain, Sweden, Switzerland and the United Kingdom. Canada is a Cooperating State. ESOC, Darmstadt, Germany. In the words of its Convention: the purpose of the Agency shall be to provide for ESRIN, Frascati, Italy. and to promote, for exclusively peaceful purposes, cooperation among European States in space research and technology and their space applications, with a view ESAC, Madrid, Spain. to their being used for scientific purposes and for operational space applications systems: Chairman of the Council: D. Williams → by elaborating and implementing a long-term European space policy, by Director General: J.-J. Dordain recommending space objectives to the Member States, and by concerting the policies of the Member States with respect to other national and international organisations and institutions; → by elaborating and implementing activities and programmes in the space field; → by coordinating the European space programme and national programmes, and by integrating the latter progressively and as completely as possible into the European space programme, in particular as regards the development of applications satellites; → by elaborating and implementing the industrial policy appropriate to its programme and by recommending a coherent industrial policy to the Member States.
    [Show full text]
  • Launch of the PROBA-2 Satellite: Another Success for NGC Aerospace
    PRESS RELEASE November 2, 2009 Launch of the PROBA-2 satellite: another success for NGC Aerospace On November 2 nd , 2009 at 1:50 am Greenwich mean time (7:50 pm on November 1st in Sherbrooke), the PROBA-2 satellite began its two-year space journey to accomplish its dual mission of scientific discovery and technology demonstration. Launched from the Plesetsk Cosmodrome in Russia, the 130 kg satellite was successfully placed on its sun- synchronous orbit at an altitude of 700 km. PROBA-2, which is the size of a large television and consumes the energy equivalent to a 60 Watt bulb, has four scientific experiments on board (two in the field of space weather and two for sun observation) as well as 17 technological innovations that will be validated in orbit. Involved in the project since 2004, Sherbrooke-based NGC Aerospace participated in the design and implementation of PROBA-2 by providing the software that controls the attitude and orbit of the satellite in accordance with the requirements of the scientific mission. Thus, it is the computer software designed by NGC which orients the spacecraft so its cameras and scientific instruments can acquire their data with the accuracy and the stability required by the mission scientists. In addition, thanks to its participation in the project, NGC will have the opportunity to validate in orbit, in the context of a real space mission, up to six different technological innovations, ranging from the measurement of the satellite temperature to determine its position above the ground to using the Earth's magnetic field to orient the spacecraft in the desired direction.
    [Show full text]
  • Espinsights the Global Space Activity Monitor
    ESPInsights The Global Space Activity Monitor Issue 6 April-June 2020 CONTENTS FOCUS ..................................................................................................................... 6 The Crew Dragon mission to the ISS and the Commercial Crew Program ..................................... 6 SPACE POLICY AND PROGRAMMES .................................................................................... 7 EUROPE ................................................................................................................. 7 COVID-19 and the European space sector ....................................................................... 7 Space technologies for European defence ...................................................................... 7 ESA Earth Observation Missions ................................................................................... 8 Thales Alenia Space among HLS competitors ................................................................... 8 Advancements for the European Service Module ............................................................... 9 Airbus for the Martian Sample Fetch Rover ..................................................................... 9 New appointments in ESA, GSA and Eurospace ................................................................ 10 Italy introduces Platino, regions launch Mirror Copernicus .................................................. 10 DLR new research observatory ..................................................................................
    [Show full text]
  • Instructions to Authors for the Preparation of Papers
    PROBA-V: AN OPERATIONAL AND TECHNOLOGY DEMONSTRATION MISSION – RESULTS AFTER COMMISSIONING AND ONE YEAR OF IN-ORBIT EXPLOITATION K. Mellab(1), S. Santandrea(1), M. Francois(1), D. Vrancken(5), D. Gerrits(5), A. Barnes(1), P.Nieminen(1), P. Willemsen(1), S. Hernandez(1), A. Owens(1), T. Delovski(2), M. Cyamukungu(3), C.Granja(4) (1) ESA-ESTEC, Keplerlaan 1, 2201AG Noordwijk (NL) +31 71 565 3249, Email: [email protected] (2) DLR - Institute of Space Systems, Robert-Hooke-Str. 7, 28359 Bremen, Germany (3) UCL, Center for Space Radiations chemin du cyclotron 2 B-1348 Louvain-la-Neuve, Belgium (4) Institute of Experimental and Applied Physics, Horska 3a/22, 128 00 Prague 2, Czech Republic (5) QinetiQ Space nv, Hogenakkerhoekstraat 9 B-9150 Kruibeke Belgium ABSTRACT Proba-V, the third mission of ESA’s Programme for In-orbit Technology Demonstration (IOD), conceived and developed following the footsteps of its predecessors, Proba-1 and Proba-2, is an operational mission based on a small, high performance satellite platform and a compact payload, whose main aim is the continuation of the SPOT/Vegetation programme, now planned for decommissioning. Successfully launched by the ESA VEGA launcher in May 2013, it has completed its commissioning and the full calibration of platform, main instrument and additional payloads and is, since last October, fully operational. The development of the Vegetation Instrument, the main satellite’s instrument, required the use of a number of innovative technologies, in order for it to be compatible with a small platform’s resources, while at the same time being able to enhance Vegetation images’ resolution performances from 1km to 100m at Nadir.
    [Show full text]
  • IFC-AMC Motion to Dismiss
    Case 1:17-cv-01494-VAC-SRF Document 34-1 Filed 02/16/18 Page 1 of 1 PageID #: 1030 IN THE UNITED STATES DISTRICT COURT FOR THE DISTRICT OF DELAWARE JUANA DOE I et al., § § Plaintiffs, § § vs. § § C.A. No. 17-1494-VAC-SRF IFC ASSET MANAGEMENT COMPANY, § LLC, § § Defendant. § [PROPOSED] ORDER WHEREAS, Defendant IFC Asset Management Company, LLC, having moved to dismiss the claims in Plaintiff Juana Doe I et al.’s Complaint (D.I. 1); and, WHEREAS, the Court having considered the briefs and arguments in support of and in opposition to said Motion; IT IS HEREBY ORDERED this _______ day of ____________, 2018, that the Motion is GRANTED. Plaintiffs’ Complaint is dismissed with prejudice. _______________________________ United States District Judge RLF1 18887565v.1 Case 1:17-cv-01494-VAC-SRF Document 34-1 Filed 02/16/18 Page 1 of 1 PageID #: 1030 IN THE UNITED STATES DISTRICT COURT FOR THE DISTRICT OF DELAWARE JUANA DOE I et al., § § Plaintiffs, § § vs. § § C.A. No. 17-1494-VAC-SRF IFC ASSET MANAGEMENT COMPANY, § LLC, § § Defendant. § [PROPOSED] ORDER WHEREAS, Defendant IFC Asset Management Company, LLC, having moved to dismiss the claims in Plaintiff Juana Doe I et al.’s Complaint (D.I. 1); and, WHEREAS, the Court having considered the briefs and arguments in support of and in opposition to said Motion; IT IS HEREBY ORDERED this _______ day of ____________, 2018, that the Motion is GRANTED. Plaintiffs’ Complaint is dismissed with prejudice. _______________________________ United States District Judge RLF1 18887565v.1 Case 1:17-cv-01494-VAC-SRF Document 35 Filed 02/16/18 Page 1 of 51 PageID #: 1031 IN THE UNITED STATES DISTRICT COURT FOR THE DISTRICT OF DELAWARE JUANA DOE I et al., § § Plaintiffs, § § vs.
    [Show full text]