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MANUEL DE LA MISSION Manuel De La Mission Expedition 2395 2 SOMMAIRE

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MANUEL DE LA MISSION Manuel De La Mission Expedition 2395 2 SOMMAIRE EXPEDITION 35 MANUEL DE LA MISSION Manuel de la mission Expedition 2395 2 SOMMAIRE L'EQUIPAGE ­ La présentation ­ Le Timeline 4 LE VAISSEAU ­ Le vaisseau Soyuz 8 LE LANCEMENT ­ Les horaires ­ Le planning 10 ­ La chronologie de lancement LA MISSION ­ L'amarrage ­ La présentation 16 LE RETOUR ­ L'atterrissage 18 3 Manuel de la mission Expedition 35 L'EQUIPAGE LA PRESENTATION Chris A. HADFIELD (commandant de bord) Etat civil: Date de naissance: 18/08/1959 Lieu de naissance: Sarnia (Canada) Statut familial: Marié et 3 enfants Etudes: Bâchelier en ingénierie mécanique (Royal Military College), Maîtrise dans les systèmes avioniques (University of Tennessee) Statut professionnel: Chef des astronautes canadiens et NASA Director of Operations au centre d'entraînement russe CSA: Sélectionné comme cosmonaute le 09/06/1992 (CSA­2) Précédents vols: STS­74 (08 jours 04:31 en novembre 1995) STS­100 (11 jours 21:31 d'avril à mai 2001) Roman Y. ROMANENKO (ingénieur de vol) Etat civil: Date de naissance: 09/08/1971 Lieu de naissance: Shchelkovo (Russie) Statut familial: Marié et 2 enfants Etudes: Graduat comme pilote (Chernigov Higher Military Air School of Pilots) Statut professionnel: Colonel à l'Armed Forces of the Russian Federation retraité Roskosmos: Sélectionné comme cosmonaute le 28/07/1997 (TsPK­12) Précédents vols : Expedition 20/21 (187 jours 20:42 de mai à décembre 2009) Manuel de la mission Expedition 35 4 L'EQUIPAGE Thomas H. MARSHBURN (ingénieur de vol) Etat civil: Date de naissance: 29/08/1960 Lieu de naissance: Statesville (Caroline du Nord) Statut familial: Marié et 1 enfant Etudes: Bachelier en physique (Davidson College), Maîtrise en physique (University of Virginia), Doctorat en médecine (Wake Forest University), Maîtrise en science médicale (University of Texas Medical Branch) Statut professionnel: Médecin urgentiste (Johnson Space Center) Nasa: Sélectionné comme astrononaute le 06/05/2004 (Groupe 19) Précédents vols : STS­127 (15 jours 16:45 en juillet 2009) Pavel V. VINOGRADOV (ingénieur de vol) Etat civil: Date de naissance: 31/08/1953 Lieu de naissance: Magadan (Russie) Statut familial: Marié et 3 enfants Etudes: Graduat comme pilote (Moscow Aviation Institute) Statut professionnel: Chef du RKKE Flight Test Center Roskosmos: Sélectionné comme cosmonaute le 03/03/1992 (NPOE­10) Précédents vols : Mir 24 (197 jours 17:34 d'août 1997 à février 1998) Expedition 13 (182 jours 22:43 de mars à septembre 2006) 5 Manuel de la mission Expedition 35 L'EQUIPAGE Alexsandr A. MISURKIN (ingénieur de vol) Etat civil: Date de naissance: 23/09/1977 Lieu de naissance: Yershichi (Russie) Statut familial: Marié et 1 enfant Etudes: Graduat comme pilote d'essai (Kacha High Air Force Pilot School), Graduat comme pilote ingénieur (Armavir Military Aviation Institute) Statut professionnel: Lieutenant­colonel à la Russian Air Force retiré Roskosmos: Sélectionné comme cosmonaute le 11/10/2006 (TsPK­14) Précédents vols: ­ Christopher J. CASSIDY (ingénieur de vol) Etat civil: Date de naissance: 04/01/1970 Lieu de naissance: Salem (Massachusetts) Statut familial: Marié et 3 enfants Etudes: Bachelier en mathématique (U.S. Naval Academy), Maîtrise en océanographie (MIT) Statut professionnel: Lieutenant Commander (US Navy) Nasa: Sélectionné comme astrononaute le 06/05/2004 (Groupe 19) Précédents vols : STS­127 (15 jours 16:45 en juillet 2009) Manuel de la mission Expedition 35 6 L'EQUIPAGE LE TIMELINE Expedition 35 est composé de deux groupes : Groupe A (Hadfield, Romanenko, Marshburn) Expedition 34 du 19/11/2012 au 14/03/2013 Expedition 35 du 14/03/2013 au 14/05/2013 Départ: 17/11/2012 à bord de Soyuz TMA­07M A bord de l'ISS: 17/11/2012 au 14/05/2013 Retour: 14/05/2013 à bord de Soyuz TMA­07M Groupe B (Vinogradov, Misurkin, Cassidy) Expedition 35 du 28/03/2013 au 14/05/2013 Expedition 36 du 14/05/2013 au 11/09/2013 Départ: 28/03/2013 à bord de Soyuz TMA­08M A bord de l'ISS: 28/03/2013 au 11/09/2013 Retour: 11/09/2013 à bord de Soyuz TMA­08M 01 /201 3 11/2012 12/2012 02/2013 03/2013 04/2013 05/2013 06/2012 07/2013 Groupe A H. Groupe A R. Groupe A M. Groupe B V. Groupe B M. Groupe B C. Expedition 34 (19/11/2012 ­ 14/03/2013) Expedition 35 (14/03/2013 ­ 14/05/2013) Expedition 36 (14/05/2013 ­ 11/09/2013) 7 Manuel de la mission Expedition 35 LE VAISSEAU LE VAISSEAU SOYUZ Bien qu’il vole depuis 1967, le vaisseau Soyuz n’est pas démodé pour autant. Au fil des ans, il a subi des modifications, notamment suite aux accidents de Soyuz 1 en 1967 (parachutes qui se sont mal déployés lors du retour sur Terre) et Soyuz 11 (dépressurisation lors du retour sur Terre), mais aussi un lifting. Dans sa première version, Soyuz a volé jusqu’en 1981. Dans la version T, il s’est amarré aux différentes stations spatiales Salyut de 1980 jusqu’à l’arrivé de Mir en 1986. A cette date, c’est la version TM qui a pris le relais puis TMA à partir de 2002. Depuis décembre 2011, seule la version numérique de Soyuz TMA est utilisée, à savoir Soyuz TMA M. Soyuz en chiffres : Masse au décollage : 7 250 kg Nombre de passagers : 3 avec combinaison spatiale Largeur : 10,6 m panneaux solaires déployés (2,7 m non déployés) Hauteur : 7,2 m Volume habitable : +/­ 10 m³ Manuel de la mission Expedition 35 8 LE VAISSEAU Module orbital Module orbital quasi sphérique (2,2 m de diamètre pour 2,6 m de haut) pesant environ 1 300 kg. Il est situé au sommet du vaisseau et comprend les antennes et le collier d’amarrage. L’équipage s’en sert pour se dégourdir les jambes entre le lancement et l’amarrage quelques 48 heures plus tard environ. Dans ce module, on y entrepose une partie du matériel, effets personnels et diverses expériences, soit une masse de 230 kg maximum. Module de descente Module dans lequel l’équipage est assis au moment du lancement et de l’atterrissage. C’est la seule partie qui revient sur Terre, protégée par un bouclier thermique largable en vol. Il mesure 2,1 m de haut pour 2,2 m de diamètre. Il pèse quelques 2 900 kg. Il peut également transporter des effets personnels, à concurrence de 50 kg pour 3 personnes. Module technique et de propulsion Cylindre de 2,5 m de haut pour 2,7 m de diamètre à la base. On y retrouve les moteurs, les réservoirs de carburants et les panneaux solaires. 9 Manuel de la mission Expedition 35 LE LE ANCEMENT LES HORAIRES 27/03: Présentation de l'équipage à la Commission d'Etat (19:00 TU) 28/03: Début de la retransmission en direct du lancement (19:30 TU) ­ lancement à 20:43 TU 28/03: Conférence post­lancement (23:00 TU) 29/03: Début de la retransmission de l’amarrage à l’ISS (01:30 TU) – amarrage à 02:32 TU 29/03: Début de la retransmission de l’ouverture des écoutilles (04:10 TU) Les horaires sont sujets à modification. Pour ne rien rater des évènements, regardez le programme à l’adresse suivante : http://www.nasa.gov/multimedia/nasatv/MM_NTV_Breaking.html Manuel de la mission Expedition 35 1 0 LE LE ANCEMENT LA CHRONOLOGIE DU LANCEMENT Chronologie finale et étapes de lancement typiques pour une mission habitée à bord de Soyuz H0 – 34:00:00 Préparation du lanceur pour le remplissage en kérosène et oxygène liquide H0 – 06:00:00 Début du compte à rebours final Batteries installées sur le lanceur H0 – 05:30:00 La Commission d’état donne le feu vert pour le lancement H0 – 05:15:00 Arrivée de l’équipage sur le site 254 H0 – 05:00:00 Remplissage en ergols de la fusée H0 – 04:20:00 Habillage de l’équipage 11 Manuel de la mission Expedition 35 LE LE ANCEMENT H0 – 04:00:00 Remplissage en oxygène liquide terminé H0 – 03:40:00 Rencontre des délégations par l’équipage H0 – 03:10:00 Rapports de la Commission d’état H0 – 03:05:00 Transfert vers le pas de tir H0 – 03:00:00 Remplissage des réservoirs terminés H0 – 02:35:00 Arrivée de l’équipage du le pas de tir H0 – 02:30:00 Embarquement de l’équipage H0 – 02:00:00 Embarquement de l’équipage terminé H0 – 01:55:00 Fermeture des écoutilles H0 – 01:45:00 Test des logiciels de rentrée Ventilation des combinaisons H0 – 00:01:30 Ecrans de commande de lancement et l’unité d’approvisionnement sont préparés Fermeture du sas et test d’étanchéité du vaisseau H0 – 00:01:00 Préparation du système de contrôle du lanceur Activation des centrales inertielles H0 – 00:45:00 Les structures de service du pas de tir reçoivent l’ordre de repli H0 – 00:40:00 Test des logiciels de rentrée terminé. Contrôle de la pressurisation des combinaisons H0 – 00:30:00 Fusée de sauvetage armée Fin du chargement du plan de vol H0 – 00:25:00 Les tours de services sont repliées en mode lancement Manuel de la mission Expedition 35 1 2 LE LE ANCEMENT H0 – 00:15:00 Fin du contrôle d’étanchéité des combinaisons Evacuation du site de lancement par tout le personnel H0 – 00:10:00 Début des enregistrements des activités de l’équipage H0 – 00:07:00 Fin des opérations « Pré­lancement » H0 – 00:06:15 La clé de commande du lancement est donnée au site de lancement Le programme automatique des opérations finales de lancement est activé H0 – 00:06:00 Le complexe de lancement et le lanceur sont prêts pour la mise à feu H0 – 00:05:00 Les systèmes embarqués sont branchés sur contrôle de bord Le système de mesure au sol est activé par la commande RUN 1 Les contrôles de commandes sont activés Les cosmonautes ferment le casque de leur scaphandre La clé de lancement est insérée dans le bunker de lancement H0 – 00:03:15 Les chambres de combustion sont purgées en azote H0 – 00:02:30 Le système de mesure embarqué est branché par la commande RUN 2 Début de la pressurisation des réservoirs avec du azote H0 – 00:02:15 Les valves de remplissage sur le lanceur sont fermées H0 – 00:01:00
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