A. Novelli – Head of ATV Mission Operations
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 1 Page 1
84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 00 01 02 03 04 05 06 07 08 Phase B Freedom Redesign ISS Scrub 89 Restructuring Story Phase1 – MIR/Shuttle International Space Station - ISS
Reagan’s call Gore/Tchernomyrdin IGA/MOUs 1st crew agreement
Short Term studies Complementary study B1 B2 ATV development (C/D) Trilateral Statement ATV DMS-R/RDS Barter Story Joint Decision Exchange Of Letters Jules Verne Launch Integration Contract signature Russian Systems Contract signature ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 2 Page 2 ISS today
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 3 Page 3 The International Space Station
RUSSIA ESA-ATV
CANADA
USA JAPAN ESA-COLOMBUS
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 4 Page 4 ESA Elements on ISS
ERA MSG Microgravity Science Glovebox ATV European MSL Materials Science Laboratory (in MSRR-1) Automated Robotic Arm EMCS European Modular Cultivation System Transfer PFS Pulmonary Function System (in HRF-2) Vehicle DMS-R ESA's Data Management System for the Russian Segment of the ISS. Located in service module Zvezda.
Node 3 Connecting Module Cupola Pressurised observation and Node 2 work area Connecting Module MELFI -80°C Freezer for research specimens. Columbus Located in Destiny or (Biolab, FSL, EPM, EDR with PCDF, Kibo MARES, EuTEF, SOLAR, ACES)
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 5 Page 5 Automated Transfer Vehicle (ATV)
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 6 Page 6 Operations
ATV Control-Centre, Toulouse (F)
Columbus Control-Centre, Munich (D) • COL-CC is now in full operations since 2007 • ATV-CC has successfully performed the first ATV mission and is now executing the ATV-02
operations
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 7 Page 7 ATV ground communication network
Ku-Band Fwd 3Mbps (OCA) TDRSS Rtn 50Mbps ISS
ARTEMIS S-Band ATV Prox Link
S-Band
ARTEMIS ATV
REDU EET
ESA G/W ESA G/W TDRSS TsUP WSGT POIC & Russian PDSS MCC-M GS
N/W HOSC G/WESA ESA IGS cloud ESA G/W Mgt & Control European Astroaut NISN SSCC Centre IGS Central Node MCC-H G/WESA and NetworkServices IGS Node Data, Voice & Video IGS Node IGS Node Services ESA MSM Columbus Communications A5 GSC ATV Infrastructure Kourou USOCs ATV-CC Columbus-CC ESCs
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 8 Page 8 ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 Page 9 Mission Overview
ATVISS 2004-03 Johannes Kepler docking TsUP/KorolevATV-CC – 24 –th24Februaryth February 2011 2011 10 Page 10
ATV Mission altitude profile
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 11 Page 11 ATV Rendez-vous
Station keeping
CoM distances - 3500 m - 250 m AE V 30 km KOS
S3 S2
Pre- homing Homing Closing FA
S S S-1/2 0 1 R
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 12 Page 12 Timeline ATV-02 15:22-15:58 16:37-16:42 In Centr. European 14:09-14:42 16:22-16:35 16:46 Time
MSU CM
FCM DPVt Telegoniometers
Absolute GPS GNC RGPS Videometers Docking
IF ESCAPE/CAM
S2 S3 S4 S41
~39 km ~15 km -3.5 km -249 m -19 m -11 m S -1/2 S1
Safety is guaranteed by ATV Safety is guaranteed by if ATV is within S-1/2 box ESCAPE/CAM availability
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 Page 13 Rendez-vous – Crew monitoring
Crew monitoring: during closing and final approach –Independent safety level –Dedicated video camera on aft end of Russian service module –Dedicated hardware control panel to send discrete commands to ATV
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 14 Page 14 ATV to ISS propulsive support
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 15 Page 15 Automated Transfer Vehicle Johannes Kepler performances
ATV2 will deliver to ISS ATV-2 ATV-1 2534Kg more than its Fluid Cargo Loading [kg] [kg]
predecessor ATV1 Jules Mission Propellant 2030 3598 Verne. ISS Propulsive Support 4535 2260 Water 0 267 Gas (3 tanks: Oxygen) 100 20 Refuel Propellant 850.6 860 Total Fluid Cargo 5486 3407 Dry Cargo Loading Nominal Load Cargo (Integrated 17 Sep 2010) 1170 1150 No late Late Load Cargo 435 load for (Integrated 28-29 Jan 2011) ATV-1 Total Dry Cargo 1605 1150 Total Cargo Fluid + Dry 7091 4557
ATVATISSV 2004-03 JohannesJohannes KeplerKepler dockingdocking ATV-CC – 24th February 2011 16 Page 16 Automated Transfer Vehicle Johannes Kepler Cargoes
Cargo Type Mass Utilization 204.58 Spares 555.59 Supplies (hygiene, 181.72 batteries, cleaning) Tools 26.52 Clothing 48.09 Food 519.94 PR Items 14.73 Geoflow2 Other 54.18 Columbus Power Distribution Unit Total 1605.35 (PDU)
ATVATISSV 2004-03 JohannesJohannes KeplerKepler dockingdocking ATV-CC – 24th February 2011 17 Page 17 ATV de-orbit and re-entry
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 18 Page 18 Back –up slides
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 Page 19 Automated Transfer Vehicle Made up of a an unpressurised module for propellant, water (ATV) : and gas, and a pressurised cargo carrier for dry cargo. Technical description First ATV launched by Ariane 5 from Kourou on 9 March. 08. First operational flight (Jules Verne): Launch 9 March 2008 After 25 days of autonomous transfer flight (including Docking 3 April 2008 demonstration mission), Jules Verne arrived at the De-docking 5 Sept. 2008 International Space Station and docked automatically to rear Re-entry 29 Sept. 2008 of Russian Service Module (Zvezda) on the 3rd April 2008. Second operational flight (Johannes Kepler) Launch 16 Feb. 2011 Generic ATV can carry a total cargo of up to 9 t: Docking 24 Feb. 2011 • up to 5.5 t of dry cargo De-docking 4 June 2011 (re-supply goods, scientific payload, etc) Operational flight rate: • up to 840 kg of water and 100 kg gas approximately 1 flight/15 months • up to 860 kg of propellant for refuelling the Station • up to 4.7 t of propellant for ISS propulsive support (reboost, attitude Overall length 10.3 m, control, debris avoidance manœuvre). diameter 4,5 m,
Total launch mass up to 20.7 t, with up to 9 t of gross cargo.
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 20 Page 20 Additional ESA-provided Elements
Node 2 Super Data Microgravity -80° CFreezer (NASA) Guppy Management for Science (MELFI ) (NASA Glovebox (NASA) Zvezda and JAXA ) Delivered (Roskosmos) (NASA) June 2003 Delivered FM 1 delivered On-orbit since On-orbit since October March 2002 July 2000 July 2002 to fly on ULF1.1 1997 FM 2 delivered July 2004
European Cupola Hexapod Robotic Arm Node 3 (NASA) Crew (Roskosmos) (NASA) (NASA) Refrigerator/ Delivered Freezer Delivery to Delivered Storage early 2007 (NASA) Russia May ’06 September 2005-2008
Launch with 2004 QM delivered MLM 2009 September ’05 FM Cancelled ATVATISSV 2004-03 JohannesJohannes KeplerKepler dockingdocking ATV-CC – 24th February 2011 21 Page 21 ATV technical data Launch Configuration Payload 2 x 0.314 m3 and 2 x 0.414 m3 for each envelope of 8 racks Cargo mass Dry cargo: 1500-5500 kg Water: 0-840 kg Gas (Nitrogen, Oxygen, air, 2 gasses/flight): 0-100 kg ISS re-boost and attitude control propellant: 0-4500 kg Total net cargo upload capacity:7667 kg
Launch vehicle Ariane 5 (260x260 km, 51.6° transfer path)
ATV will be launched with its solar panels folded to the body of the spacecraft. Electrical power will be supplied by non rechargeable batteries. Launch site Kourou, French Guiana
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 22 Page 22 Vehicle comparison
HTV ATV Progress M1 Apollo CSM
Length 9.2m 10.3 m 7.4 m 11.03 m
Maximum Diameter 4.4 4.51 m 2.70 m 3.90 m
Launch Mass 16500kg 20750 kg 7150 kg 30329 kg
Pressurized Volume 14 m3 (+16 m3 14 m3 6.6 m3 6.17 m3 unpressurized) Cargo Upload Capacity 6000kg 7667kg 2230-3200kg Lunar mission
Engine Thrust 4x500N = 2000N 4x490 N = 1960N 2942 N 1x97860 N
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 23 Page 23 Docking system
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 24 Page 24 Optical guidance
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 25 Page 25 Docking system probe deployment
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 26 Page 26 Cargoes integration and cleaning
ATVISS 2004-03 Johannes Kepler docking ATV-CC – 24th February 2011 27 Page 27