The ATV Programme "Jules Verne"
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1 Nicholas Camussy The ATV Programme "Jules Verne" Ein Vortrag organisiert vom VDI in Kooperation mit DGLR und RAeS Hochschule für Angewandte Wissenschaften Hamburg Download:
2 ATV what s that? ATV: Automated Transfer Vehicle European Resupply spaceship to the International Space Station (ISS) First prototype / flight model dubbed Jules Verne. Mission successfully performed in 2008 Follow-up mission (Johannes Kepler) in 2010 Developed by EADS ASTRIUM for the European Space Agency (ESA) Development phase including Jules Verne s mission Production phase for additional 4 to 6 vehicles including mission
3 International Space Station (ISS) Unity and Svezda ISS
4 Mission started in Kourou (French Guiana)
5 Automated approach to the ISS
6 Another few meters to go.
7 Solidly docked to the ISS
8 Inhabited ATV in space
9 Tug / pusher for the ISS
10 Fatal splash down in the upper atmosphere
11 ATV missions ISS refueling ISS attitude control Debris avoidance Water and gas ISS attitude control Gyrodynes / GMG desaturation Dry cargo Waste destruction
12 Houston Control Center ATV system TM TC Video TDRSS ARTEMIS ATV Guiana Space Center Kourou ISS Ground network COL- CC Russian ground stations Moscow Mission Control Center TM TC Via GSFC ProxLink ATV Control Center (CNES - Toulouse)
13 ASTRIUM is ATV prime contractor Program management (relationships with ESA and numerous industrial subcontractors) System engineering On-board software development and tests Integration and tests of the spaceship Launch campaign in Kourou Development of the system operational reference Users manuals, vehicle and mission control procedures
14 10,3 m ATV Jules Verne characteristics Mass at lift off: kg Dry mass : kg Cargo delivered to ISS : 4600 kg (water, oxygen, fuel, dry cargo) 4,5 m
15 Space bus!
16 Family story!
17 Integrated Cargo Carrier Thales Alenia Space (Italy) Russian Docking system (RSC Energya Russia) Pressurised module (46 m 3 ) Non pressurised module Dry cargo: 1150 kg Water: 270 kg Oxygen: 21 kg Fuels: 856 kg
18 Spacecraft Avionics bay (ASTRIUM) Propulsion bay (ASTRIUM) 28 engines 220 N 4 engines 490 N Fuels (MMH and MON): kg (mission and reboost) Solar panels (4 wings Dutch Space ) 22 meter wingspan 4,8 kw beginning of life
19 A true European system! DNV SAAB DUTCH SPACE ETS BRADFORD ROVSING SAS / ABSp / EHP ASTRIUM Space Transp. ASTRIUM Satellites SODERN / CLEMESSY Thales Alenia Sp. / SAFT SNECMA IBERESPACIO CASA / CRISA / RYMSA Thales Espacio Major subcontractor in Russia (RSC-E): Docking and refuelling subsystems Subcontractors in the US: Perkin Elmer, Aerojet, Vacco TESAT ASTRIUM Space Transp. JOP / OHB / MAN FRIWO CONTRAVES SPACE HTS / APCO TECH. Syderal Thales Alenia Space DATAMAT DATASPAZIO Galileo Av. / LABEN/ FIAT
20 Structural model (ESTEC September 2002)
21 Jules Verne EMC tests (ESTEC 2004)
22 Jules Verne Solar wings deployment tests (ESTEC 2005)
23 Jules Verne Acoustic tests (ESTEC June 2006)
24 Jules Verne Thermal vacuum tests (ESTEC December 2006)
25 Functional qualification tests Les Mureaux
26 Altitude (km) Mission profile Time Launch ( ) Pre-launch
27 Altitude (km) Low earth orbit ops (LEOP) LEOP Phasing with ISS Launch ( ) Deployment of telecommunication antennas Acquisition of TDRSS communication link Deployment of solar wings Initialisation of the propulsion subsystem GPS system initialisation First on-orbit manoeuvres / demonstrations Temps Pre-launch
28 Prepare to docking (1) The ISS is inhabited (3 astronauts on-board as of today) and ATV had to demonstrate safety of operations before docking 14 March 2008: Demonstration of contingency procedures ATV loitering far behind the ISS Triggering of a Collision Avoidance Manoeuvre (CAM) Fully automated sequence Escape from the ISS managed by a contingency system (dedicated computer and engines.) Survival mode (zero fault tolerance) and exit from survival Manoeuvre successfully executed on first run and without anomalies 15 to 19 March 2008: Transfer to parking orbit
29 Prepare to docking (2) 20 to 28 March 2008 ATV loitering far behind the ISS Waiting for the US space shuttle to dedock from ISS (no simultaneous ops) 29 March 2008: Demo Day 1 Approaching the ISS at 3,5 km Relative GPS navigation between ATV and ISS (world premiere) Direct communication link between ATV and ISS Manoeuvre completed by issuing an «Escape» command 31 March 2008: Demo Day 2 Approaching the ISS at 11 km Use of the optical rendez-vous sensors (world premiere) Vehicle controlled by the ISS crew and the ATV control centre Ready for docking!
30 Demonstration day 1 ( ) S2 (3,5 km) S -1/2 (30 km) Escape (triggered by ATV-CC)
31 Demonstration day 2 ( ) S3 S2 (300 m) (3,5 km) (100 m) Retreat (1) S4.1 S4 (12 m) (20 m) Resume (1) Hold (1) Retreat (1) Escape (2) 1 : Triggered by ATV-CC 2 : Triggered by ISS crew
32 Rendezvous Altitude (km) Not to scale S 0 S 1 Mission scenario S 2 S 4 S 3 S 41 Docking Time Phasing Launch ( ) Pre-launch
33 Rendez-vous and docking Absolute GPS navigation Long range
34 Rendez-vous and docking Hyper frequency link with the ISS Absolute GPS Relative GPS 5 km -30 km S 0 Long range
35 Rendez-vous and docking Orbit raising manoeuvre to reach the ISS -30 km -15 km S 0 S 1 Long range
36 Rendez-vous and docking Activation KURS and ranging cues KURS transponder (second trasnponder on ATV rear side) S 2-30 km -15 km -3.5 km S 0 S 1 Long range
37 Rendez-vous and docking Videometers Telegoniometers S 2 S 3-30 km -15 km S 0 S km -249 m Transition from FAR to CLOSE RANGE sensors Far Range Close Range
38 Rendez-vous and docking Visual Video Target and Russian cameras system Monitoring by crew S 2 S 3-30 km -15 km S 0 S km -249 m Transition from FAR to CLOSE RANGE sensor Far Range Close Range
39 Rendez-vous and docking Visual Video Target and Russian cameras system Monitoring by crew Commanding S 2 S 3-30 km -15 km S 0 S km -249 m Transition from FAR to CLOSE RANGE sensor Far Range Close Range
40 Rendez-vous and docking Primarily composed of RGPS data (from 30 km to S 3 (249m)) and VDM data (from S 3 to Docking) Close RVDM S 2 S 3 S 4 KURS data -30 km -15 km S 0 S km -249 m -19 m Far Range Close Range
41 Rendez-vous and docking phase S 2 S 3 S 4 S km -15 km S 0 S km -249 m -19 m -11 m Far Range Close Range
42 Rendez-vous and docking phase S 2 S 3 S 4 S km -15 km S 0 S km -249 m -19 m -11 m DOCKING Far Range Close Range
43 Rendezvous Altitude (km) Not to scale S 0 S 1 Mission profile S 2 S 4 S 3 S 41 Docking Time Phasing Launch Pre-Launch
44 Rendezvous Altitude (km) Not to scale S 0 S 1 Mission profile S 2 S 4 S 3 S 41 Docking Time Attached Phase Phasing Launch Pre-Launch
45 On-orbit ops Payload transfer Water, gas, ISS refuelling propellants Dry cargo ATV loaded with wastes Propulsive support to ISS Reboost Attitude and orbit control (debris avoidance manoeuvre / DAM) Rest place for the astronauts! All operations performed as planned, no anomalies
46 ISS reboost by ATV 25 avril 12 juin 08 juillet 06 août 07 août
47 Time Dedocking Rendez-vous Altitude (km) S 0 S 1 S 2 Dedocking Attached phase Reboost S 4 S 3 S 41 Docking Phasing with ISS Launch ( ) Pre-launch
48 Time Reentry ( ) Deorbitation ( ) Dedocking ( ) Rendezvous Altitude (km) Deorbitation and reentry Attached phase Phasing with ISS Launch ( ) Reboost S 0 S 2 S 4 S 1 S 3 S 41 Docking Pre-launch
49 What s next? Successful mission from launch until reentry By far, most complex space mission performed in Europe No failure of any equipment or subsystem No upload of software patch necessary Several «world premieres» performed during this inaugural flight Extraordinary human adventure for European teams in permanent interface with counterparts in the US and in Russia Extraordinaire competencies developed in Europe, paving the way for further evolutions Non destructive reentry (download of samples from the ISS) Manned flights Planetary exploration
50 ISS as seen from 16 Februar the 2009 US space shuttle.
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