5 Years Experience of Columbus Ground Segment Operations
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Soyuz TMA-11 / Expedition 16 Manuel De La Mission
Soyuz TMA-11 / Expedition 16 Manuel de la mission SOYUZ TMA-11 – EXPEDITION 16 Par Philippe VOLVERT SOMMAIRE I. Présentation des équipages II. Présentation de la mission III. Présentation du vaisseau Soyuz IV. Précédents équipages de l’ISS V. Chronologie de lancement VI. Procédures d’amarrage VII. Procédures de retour VIII. Horaires IX. Sources A noter que toutes les heures présentes dans ce dossier sont en heure GMT. I. PRESENTATION DES EQUIPAGES Equipage Expedition 15 Fyodor YURCHIKHIN (commandant ISS) Lieu et Lieu et date de naissance : 03/01/1959 ; Batumi (Géorgie) Statut familial : Marié et 2 enfants Etudes : Graduat d’économie à la Moscow Service State University Statut professionnel: Ingénieur et travaille depuis 1993 chez RKKE Roskosmos : Sélectionné le 28/07/1997 (RKKE-13) Précédents vols : STS-112 (07/10/2002 au 18/10/2002), totalisant 10 jours 19h58 Oleg KOTOV(ingénieur de bord) Lieu et date de naissance : 27/10/1965 ; Simferopol (Ukraine) Statut familial : Marié et 2 enfants Etudes : Doctorat en médecine obtenu à la Sergei M. Kirov Military Medicine Academy Statut professionnel: Colonel, Russian Air Force et travaille au centre d’entraînement des cosmonautes, le TsPK Roskosmos : Sélectionné le 09/02/1996 (RKKE-12) Précédents vols : - Clayton Conrad ANDERSON (Ingénieur de vol ISS) Lieu et date de naissance : 23/02/1959 ; Omaha (Nebraska) Statut familial : Marié et 2 enfants Etudes : Promu bachelier en physique à Hastings College, maîtrise en ingénierie aérospatiale à la Iowa State University Statut professionnel: Directeur du centre des opérations de secours à la Nasa Nasa : Sélectionné le 04/06/1998 (Groupe) Précédents vols : - Equipage Expedition 16 / Soyuz TM-11 Peggy A. -
Attachment J-4 Applicable and Reference Documents Lists
NNJ12GA46C SECTION J Attachment J-4 MISSION AND PROGRAM INTEGRATION CONTRACT Attachment J-4 Applicable and Reference Documents Lists J-A4-1 NNJ12GA46C SECTION J Attachment J-4 MISSION AND PROGRAM INTEGRATION CONTRACT This attachment contains applicable documents for the contract effort. The contractor shall comply with these requirements in performing Statement of Work (SOW) requirements. This attachment is structured as follows: Table J4-1: Applicable Documents List Table J4-2: Reference Documents List Table J4-3: Book Editor/Book Coordinated/Managed Documents List Table J4-4: Orion Documents List The documents identified within Table J4-1 or within a document listed in this table (second tier) are applicable to this contract. Requirements written in these documents have full force and effect as if their text were written in this contract to the extent that the requirements relate to context of the work to be performed within the scope of this contract. When a document is classified as “reference,” the document is provided for information about the ISS Program execution and the Mission and Program Integration Contract’s role in the ISS Program. The general approach for interpreting whether a document impacts the contractor’s performance is that if a document is “applicable,” then the contractor has solid requirements that derive from that document. Applicable documents contain additional requirements and are considered binding to the extent specified. Applicable documents cited in the text of the document in a manner that indicates applicability such as follows: • In accordance with • As stated in • As specified in • As defined in • Per • In conformance with When a document is classified as “reference,” the document is provided for general context of the ISS Program execution and for influence on the performance of the Mission and Program Integration Contract in its role of support to the ISS Program. -
Analysis of Narrow-Line Laser Cooling and Trapping of Sr Atoms in Microgravity Environments
applied sciences Article Analysis of Narrow-Line Laser Cooling and Trapping of Sr Atoms in Microgravity Environments Jie Ren 1,2, Hui Liu 3,* , Xiaotong Lu 1,2 and Hong Chang 1,2,* 1 CAS Key Laboratory of Time and Frequency Primary Standards, National Time Service Center, Xi’an 710600, China; [email protected] (J.R.); [email protected] (X.L.) 2 School of Astronomy and Space Science, University of Chinese Academy of Sciences, Beijing 100049, China 3 State Key Laboratory of Photoelectric Technology and Functional Materials, International Collaborative Center on Photoelectric Technology and Nano Functional Materials, Institute of Photonics & Photon-Technology, Northwest University, Xi’an 710069, China * Correspondence: [email protected] (H.L.); [email protected] (H.C.) Received: 7 June 2020; Accepted: 15 July 2020; Published: 17 July 2020 Abstract: Obtaining ultracold alkaline earth(-like) atoms in space encounters the problem of performing narrow-line laser cooling in microgravity environments (µ-gEs). This paper reports an analysis of the magneto-optical trap (MOT) based on the narrow-line transition in 88Sr, while paying special attention to the role of the gravity. This analysis suggests the MOTs based on narrow-line transitions cannot be cold and dense enough in a µ-gE. We thus propose a strategy: that one can use a dual-frequency MOT to realize a low-temperature, high density, and high transfer efficiency, narrow-line red MOT in µ-gEs. Keywords: lasering cooling and trapping; microgravity; Monte Carlo simulation; optical lattice clocks; in space 1. Introduction Great efforts have been made in recent decades to push cold atoms into microgravity environments [1]. -
SPACE for LIFE Human Spaceflight Science Newsletter
→ SPACE FOR LIFE human spaceflight science newsletter March 2010 In this issue: - Frank de Winne on ISS - SEEDS in EXPOSE–E - Parabolic Flight no. 51 - Recent events - Dates for the Agenda Frank de Winne onboard the ISS in front of the Microgravity Science Glovebox (MSG). Courtesy of NASA ISS EXPERIMENTAL ACTIVITIES PERFORMED DURING FRANK DE WINNE’s STAY ON ISS During his stay onboard the ISS, between his arrival 29 May and departure 01 December 2009 ESA astronaut Frank de Winne in the end had a full experimental programme. Upload restrictions did at one point threaten the scientific programme, but work-arounds gave in the end almost 100% of the science that had been expect- ed. This article gives a short account of each experiment Frank de Winne performed, with special focus on the last activated experiment, the SODI-IVIDIL experiment. After its uploading onboard the 17A each end of the volume. This is a very sion in Liquids) (STS-128) mission in August 2009, the slow process when left to itself, - DSC (Diffusion Soret Coefficient) and Selectable Optical Diagnostics Instru- 2) The g-jitter, investigated for what it in - COLLOID ment (SODI) was installed as planned reality means for fluid sciences in Space, on 23 September, with a functional as this has never been substantiated, but DSC is the next one up, presently being check-out on 1 October. Five days later always been assumed to be a significant performed, with COLLOID following. the first SODI related experiment, IVIDIL problem, and The sample container – named ‘cell ar- was run for the first time. -
Jules Verne ATV Launch Approaching 11 February 2008
Jules Verne ATV launch approaching 11 February 2008 will carry up to 9 tonnes of cargo to the station as it orbits 400 km above the Earth. Equipped with its own propulsion and navigation systems, the ATV is a multi-functional spacecraft, combining the fully automatic capabilities of an unmanned vehicle with the safety requirements of a crewed vehicle . Its mission in space will resemble that, on the ground, of a truck (the ATV) delivering goods and services to a research establishment (the space station). A new-generation high-precision navigation system will guide the ATV on a rendezvous trajectory towards the station. In early April, Jules Verne will automatically dock with the station’s Russian Preview of the maiden launch and docking of ESA's Jules Verne ATV. Jules Verne will be lifted into space on Service Module, following a number of specific board an Ariane 5 launch vehicle. Credits: ESA - D. operations and manoeuvres (on 'Demonstration Ducros Days') to show that the vehicle is performing as planned in nominal and contingency situations. It will remain there as a pressurised and integral After the successful launch of ESA’s Columbus part of the station for up to six months until a laboratory aboard Space Shuttle Atlantis on controlled re-entry into the Earth’s atmosphere Thursday (7 February), it is now time to focus on takes place, during which it will burn up and, in the the next imminent milestone for ESA: the launch of process, dispose of 6.3 tonnes of waste material no Jules Verne, the first Automated Transfer Vehicle longer needed on the station. -
Level Ministerial and Scientific Event a New Era of Blue Enlightenment
Report on the High- Level Ministerial and Scientific Event A New Era of Blue Enlightenment 12-14 July 2017 Lisbon, Portugal October 2017 EUROPEAN COMMISSION Directorate-General for Research and Innovation Directorate F — Bioeconomy Unit F.4 — Marine Resources Contact: Sieglinde Gruber E-mail: [email protected] [email protected] European Commission B-1049 Brussels EUROPEAN COMMISSION Report on the High-Level Ministerial and Scientific Event A New Era of Blue Enlightenment 12-14 July 2017 Directorate-General for Research and Innovation 2017 Bioeconomy EN 3 EUROPE DIRECT is a service to help you find answers to your questions about the European Union Freephone number (*): 00 800 6 7 8 9 10 11 (*) The information given is free, as are most calls (though some operators, phone boxes or hotels may charge you) LEGAL NOTICE This document has been prepared for the European Commission however it reflects the views only of the authors, and the Commission cannot be held responsible for any use which may be made of the information contained therein. More information on the European Union is available on the internet (http://europa.eu). Luxembourg: Publications Office of the European Union, 2016. PDF ISBN 978-92-79-73529-5 doi: 10.2777/64644 KI-04-17-849-EN-N © European Union, 2017. Reproduction is authorised provided the source is acknowledged. Cover images: © Lonely, # 46246900, 2011. © ag visuell #16440826, 2011. © Sean Gladwell #6018533, 2011. © LwRedStorm, #3348265. 2011. © kras99, #43746830, 2012. Source: Fotolia.com Internal document image(s): © European Union, 2017, Source: EC - Audiovisual Service, Photo: Bruno Portela 3 "The Sea, the great unifier, is man's only hope. -
STS-134 Press
CONTENTS Section Page STS-134 MISSION OVERVIEW ................................................................................................ 1 STS-134 TIMELINE OVERVIEW ............................................................................................... 9 MISSION PROFILE ................................................................................................................... 11 MISSION OBJECTIVES ............................................................................................................ 13 MISSION PERSONNEL ............................................................................................................. 15 STS-134 ENDEAVOUR CREW .................................................................................................. 17 PAYLOAD OVERVIEW .............................................................................................................. 25 ALPHA MAGNETIC SPECTROMETER-2 .................................................................................................. 25 EXPRESS LOGISTICS CARRIER 3 ......................................................................................................... 31 RENDEZVOUS & DOCKING ....................................................................................................... 43 UNDOCKING, SEPARATION AND DEPARTURE ....................................................................................... 44 SPACEWALKS ........................................................................................................................ -
7. Operations
7. Operations 7.1 Ground Operations The Exploration Systems Architecture Study (ESAS) team addressed the launch site integra- tion of the exploration systems. The team was fortunate to draw on expertise from members with historical and contemporary human space flight program experience including the Mercury, Gemini, Apollo, Skylab, Apollo Soyuz Test Project, Shuttle, and International Space Station (ISS) programs, as well as from members with ground operations experience reaching back to the Redstone, Jupiter, Pershing, and Titan launch vehicle programs. The team had a wealth of experience in both management and technical responsibilities and was able to draw on recent ground system concepts and other engineering products from the Orbital Space Plane (OSP) and Space Launch Initiative (SLI) programs, diverse X-vehicle projects, and leadership in NASA/Industry/Academia groups such as the Space Propulsion Synergy Team (SPST) and the Advanced Spaceport Technology Working Group (ASTWG). 7.1.1 Ground Operations Summary The physical and functional integration of the proposed exploration architecture elements will occur at the primary launch site at the NASA Kennedy Space Center (KSC). In order to support the ESAS recommendation of the use of a Shuttle-derived Cargo Launch Vehicle (CaLV) and a separate Crew Launch Vehicle (CLV) for lunar missions and the use of a CLV for ISS missions, KSC’s Launch Complex 39 facilities and ground equipment were selected for conversion. Ground-up replacement of the pads, assembly, refurbishment, and/or process- ing facilities was determined to be too costly and time-consuming to design, build, outfit, activate, and certify in a timely manner to support initial test flights leading to an operational CEV/CLV system by 2011. -
SPACE for LIFE Human Spaceflight Science Newsletter July 2011
→ SPACE FOR LIFE human spaceflight science newsletter July 2011 In this issue: - ISS Science Incr. 27 end - MASER 12 in preparation - Partial-g Parabolic Flight - Mars500 one year on - Concordia Antarctica - Climate change AO - Kuipers preparing mission - Upcoming topics For full resolution of images use electronic pdf version NASA Space Shuttle STS-134 Endeavour as the last Shuttle mission with an ESA astronaut, Roberto Vittori onboard. STS-135 Atlantis closes the Shuttle era with its 8 July launch. Courtesy of NASA. Paolo Nespoli's MagISStra mission has come to an end, Roberto Vittori (ESA/ASI) has accompanied the AMS into its location on ISS Paolo nespoli touched down in Kazakhstan, together with his crew mates NASA astronaut Cady Coleman and Russian Space Agency cosmonaut Dmitry Kondratyev in their Soyuz capsule, on 23 May after a bit more than 5 months onboard the ISS, after an eventful science mission and more images of Earth taken than by any earlier ESA astronaut. ESA’s Roberto Vittori was visiting with NASA’s Space Shuttle Endeavour and the largest ISS payload ever. The Shuttle era has come to an end with the landing of STS-135 Atlantis in Florida, USA, on 21 July 2011. Paolo Nespoli started his 5 months Physical Sciences activities - last 2 months mission to the ISS mid December 2010 and concluded it with a smooth land- GeoFlow-2 experiment ing on 23 May 2011. Behind him Nespoli The GeoFlow-2 experiment, a simulation model of the left a very well done and productive movements of fluid magma near and in the crust of the job, in many cases yielding more than Earth, was under some time pressure, as the last manda- what had been expected, and not the tory run would have to be performed in time before the least producing a host of Earth images Fluid Science Lab (FSL) Video Monitoring Unit would have taken from the ISS. -
NASA Process for Limiting Orbital Debris
NASA-HANDBOOK NASA HANDBOOK 8719.14 National Aeronautics and Space Administration Approved: 2008-07-30 Washington, DC 20546 Expiration Date: 2013-07-30 HANDBOOK FOR LIMITING ORBITAL DEBRIS Measurement System Identification: Metric APPROVED FOR PUBLIC RELEASE – DISTRIBUTION IS UNLIMITED NASA-Handbook 8719.14 This page intentionally left blank. Page 2 of 174 NASA-Handbook 8719.14 DOCUMENT HISTORY LOG Status Document Approval Date Description Revision Baseline 2008-07-30 Initial Release Page 3 of 174 NASA-Handbook 8719.14 This page intentionally left blank. Page 4 of 174 NASA-Handbook 8719.14 This page intentionally left blank. Page 6 of 174 NASA-Handbook 8719.14 TABLE OF CONTENTS 1 SCOPE...........................................................................................................................13 1.1 Purpose................................................................................................................................ 13 1.2 Applicability ....................................................................................................................... 13 2 APPLICABLE AND REFERENCE DOCUMENTS................................................14 3 ACRONYMS AND DEFINITIONS ...........................................................................15 3.1 Acronyms............................................................................................................................ 15 3.2 Definitions ......................................................................................................................... -
Post Increment Evaluation Report Increment 11 International Space
SSP 54311 Baseline WWW.NASAWATCH.COM Post Increment Evaluation Report Increment 11 International Space Station Program Baseline June 2006 National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas Contract Number: NNJ04AA02C WWW.NASAWATCH.COM SSP 54311 Baseline - WWW.NASAWATCH.COM REVISION AND HISTORY PAGE REV. DESCRIPTION PUB. DATE - Initial Release (Reference per SSCD XXXXXX, EFF. XX-XX-XX) XX-XX-XX WWW.NASAWATCH.COM SSP 54311 Baseline - WWW.NASAWATCH.COM INTERNATIONAL SPACE STATION PROGRAM POST INCREMENT EVALUATION REPORT INCREMENT 11 CHANGE SHEET Month XX, XXXX Baseline Space Station Control Board Directive XXXXXX/(X-X), dated XX-XX-XX. (X) CHANGE INSTRUCTIONS SSP 54311, Post Increment Evaluation Report Increment 11, has been baselined by the authority of SSCD XXXXXX. All future updates to this document will be identified on this change sheet. WWW.NASAWATCH.COM SSP 54311 Baseline - WWW.NASAWATCH.COM INTERNATIONAL SPACE STATION PROGRAM POST INCREMENT EVALUATION REPORT INCREMENT 11 Baseline (Reference SSCD XXXXXX, dated XX-XX-XX) LIST OF EFFECTIVE PAGES Month XX, XXXX The current status of all pages in this document is as shown below: Page Change No. SSCD No. Date i - ix Baseline XXXXXX Month XX, XXXX 1-1 Baseline XXXXXX Month XX, XXXX 2-1 - 2-2 Baseline XXXXXX Month XX, XXXX 3-1 - 3-3 Baseline XXXXXX Month XX, XXXX 4-1 - 4-15 Baseline XXXXXX Month XX, XXXX 5-1 - 5-10 Baseline XXXXXX Month XX, XXXX 6-1 - 6-4 Baseline XXXXXX Month XX, XXXX 7-1 - 7-61 Baseline XXXXXX Month XX, XXXX A-1 - A-9 Baseline XXXXXX Month XX, XXXX B-1 - B-3 Baseline XXXXXX Month XX, XXXX C-1 - C-2 Baseline XXXXXX Month XX, XXXX D-1 - D-92 Baseline XXXXXX Month XX, XXXX WWW.NASAWATCH.COM SSP 54311 Baseline - WWW.NASAWATCH.COM INTERNATIONAL SPACE STATION PROGRAM POST INCREMENT EVALUATION REPORT INCREMENT 11 JUNE 2006 i SSP 54311 Baseline - WWW.NASAWATCH.COM SSCB APPROVAL NOTICE INTERNATIONAL SPACE STATION PROGRAM POST INCREMENT EVALUATION REPORT INCREMENT 11 JUNE 2006 Michael T. -
The Extreme Physical Properties of the Corot-7B Super-Earth
1 08/02/2011 The extreme physical properties of the CoRoT-7b super-Earth A. Légera,b, O. Grassetc, B. Fegleyd, F. Codrone, A., F. Albaredef, P. Bargeg, R. Barnesh, P. Cancec, S. Carpyc, F. Catalanoi, C. Cavarroca,b, O. Demangeona,b, S. Ferraz-Melloj, P. Gabora,b, J.-M. Grießmeierk, J. Leibachera,b,q, G. Libourell, A-S. Maurinl,q , S.N. Raymondl,q , D. Rouann, B. Samuela, L. Schaeferc, J. Schneidero, P. A. Schullera, F. Selsisl,q , C. Sotinp. Affiliations a. (Corresponding author) Institut d’Astrophysique Spatiale, Université Paris-Sud, bât 121, Univ. Paris-Sud, F-91405 Orsay, France; e-mail: [email protected]; ph: 33 1 69 85 85 80 b. Institut d’Astrophysique Spatiale, CNRS (UMR 8617), bât 121, Univ. Paris-Sud, F- 91405 Orsay, France, c. Université de Nantes, CNRS, Lab de planétologie et Géodynamique, UMR- CNRS 6112, F-44300 Nantes d. Planetary Chemistry Laboratory McDonnell Center for the Space Sciences, Dep. of Earth and Planetary Sciences, Washington University in St. Louis, USA; e. Laboratoire de Météorologie Dynamique CNRS/UPMC, T 45-55, E3, 75252 Paris Cedex 05 – France; f. Ecole Normale Supérieure (LST), 69364 Lyon cedex 7, France; Laboratoire d’Astrophysique de Marseille, Pôle de l'Étoile, 38 r. Frédéric Joliot-Curie, 13388 Marseille cedex 13, France g. Department of Astronomy, University of Washington, Seattle, WA, 98195-1580, USA; h. 12 av. Fontaine de la Reine, 92430 Marnes la Coquette, France; i. IAG-Universidade de Sao Paulo, Brasil; j. Centre de Biophysique Moléculaire CNRS, r. Charles Sadron, 45071 Orléans cedex 2, France; k.