head of atv mission operations february 2011...
TRANSCRIPT
Page 1ISS 2004-03ATV Johannes Kepler docking ATV-CC – 24th February 2011 1ATV Johannes Kepler docking ATV-CC –
24th
February 2011
A. Novelli –
Head of ATV Mission Operations
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84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 00 01 02 03
Reagan’s call Gore/Tchernomyrdinagreement
IGA/MOUs
Phase BFreedom
Redesign
Phase1 – MIR/Shuttle
International Space Station - ISS
Scrub 89 Restructuring
1st crew
04
Short Term studies Complementary study
B1 B2
ATV development (C/D) Trilateral Statement
Joint Decision
Exchange Of Letters
Integration Contract signature
Russian Systems Contract signature
Jules Verne Launch
ATVStory
DMS-R/RDS Barter
ISSStory
05 06 07 08
ATV Johannes Kepler docking
Page 3ISS 2004-03ATV Johannes Kepler docking ATV-CC – 24th February 2011 3
ISS today
ATV Johannes Kepler docking
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The International Space Station
ESA-COLOMBUS
JAPANUSA
CANADA
RUSSIAESA-ATV
ATV Johannes Kepler docking
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CupolaPressurised observation and work area
MELFI- 80°C
Freezer for research specimens. Located in Destiny or Kibo
ATVAutomated
Transfer Vehicle
DMS-RESA's Data
Management System for the Russian
Segment of the ISS. Located in service
module Zvezda.
Node 3Connecting Module
Node 2Connecting Module
MSG Microgravity Science Glovebox
MSL Materials Science Laboratory (in MSRR-1)
EMCS European Modular Cultivation System
PFS Pulmonary Function System (in HRF-2)
ERA European
Robotic Arm
Columbus(Biolab, FSL, EPM, EDR with
PCDF, MARES, EuTEF, SOLAR, ACES)
ESA Elements on ISS
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Automated Transfer Vehicle (ATV)
ATV Johannes Kepler docking
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Operations
ATV Control-Centre, Toulouse (F)
•
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
Columbus Control-Centre, Munich (D)
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ATV ground communication network
MCC-H
SSCC
HOSC
POIC & PDSS
N/W Mgt &
ControlNISN
WSGTTDRSS
ATV
ARTEMIS
TDRSSISS
REDU EET
ARTEMIS
Columbus-CC
IGS Central Nodeand NetworkServices
Data, Voice & Video Services
ESA
G/W
ESA
G/W
ESA G/W
MCC-M
TsUP
ESA G
/W
ATV-CC
IGS Node IGS Node
ColumbusATV
ESCs
IGS Node
USOCsA5 GSCKourou
EuropeanAstroautCentre
ESA G
/W
ESA IGS cloud
RussianGS
ESA MSMCommunications
Infrastructure
S-Band
ATV Prox Link
Ku-BandFwd 3Mbps (OCA)Rtn 50Mbps
S-Band
ATV Johannes Kepler docking
Page 9ISS 2004-03ATV Johannes Kepler docking ATV-CC – 24th February 2011
Page 10ISS 2004-03ATV Johannes Kepler docking ATV-CC – 24th February 2011 10
Mission Overview
TsUP/Korolev –
24th
February 2011ATV Johannes Kepler docking
Page 11ISS 2004-03ATV Johannes Kepler docking ATV-CC – 24th February 2011 11
ATV Mission altitude profile
ATV Johannes Kepler docking
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ATV Rendez-vous
Homing Closing FA
V
R
S2
S 1
S3
S -1/2
AE
KOS
- 250 m- 3500 m
S 0
Station keeping
30 km
Pre - homing
CoM distances
ATV Johannes Kepler docking
Page 13ISS 2004-03ATV Johannes Kepler docking ATV-CC – 24th February 2011
- 3.5 km
S3 S2
S1S-1/2
~39 km ~15 km -249 m
Telegoniometers
VideometersGNC RGPS
FCM DPVt
MSU CM
Absolute
GPS Docking
S4
-19 m
S41
-11 m
IF ESCAPE/CAM
Safety is guaranteed by ESCAPE/CAM availability
Safety is guaranteed by ATV if ATV is within S-1/2 box
14:09-14:42
15:22-15:58
16:22-16:35
16:37-16:42
16:46Timeline ATV-02In Centr. European
Time
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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
ATV Johannes Kepler docking
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ATV to ISS propulsive support
ATV Johannes Kepler docking
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Automated Transfer Vehicle Johannes Kepler performances
ATV Johannes Kepler docking
ATV2 will deliver to ISS 2534Kg more than its predecessor ATV1 Jules Verne.
45577091Total Cargo Fluid + Dry
11501605Total Dry Cargo
No late load for ATV-1
435Late Load Cargo (Integrated 28-29 Jan 2011)
11501170Nominal Load Cargo (Integrated 17 Sep 2010)
Dry Cargo Loading
34075486Total Fluid Cargo
860850.6Refuel Propellant
20100Gas (3 tanks: Oxygen)
2670Water
22604535ISS Propulsive Support
35982030Mission Propellant
ATV-1[kg]
ATV-2[kg]Fluid Cargo Loading
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Automated Transfer Vehicle Johannes Kepler Cargoes
ATV Johannes Kepler docking
Cargo TypeUtilization
Mass 204.58
Spares 555.59Supplies (hygiene, batteries, cleaning) 181.72
Tools 26.52
Clothing 48.09
Food 519.94
PR Items 14.73
Other 54.18Total 1605.35
Geoflow2Columbus Power
Distribution Unit
(PDU)
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ATV de-orbit and re-entry
ATV Johannes Kepler docking
Page 19ISS 2004-03ATV Johannes Kepler docking ATV-CC – 24th February 2011
Back –up slides
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First operational flight (Jules Verne): Launch 9 March 2008Docking 3 April 2008De-docking 5 Sept. 2008Re-entry 29 Sept. 2008
Second operational flight (Johannes Kepler) Launch 16 Feb. 2011Docking 24 Feb. 2011De-docking 4 June 2011
Operational flight rate:approximately 1 flight/15 months
Overall length 10.3 m,diameter 4,5 m,
Total launch mass up to 20.7 t,with up to 9 t of gross cargo.
Automated Transfer Vehicle (ATV) :Technical description
Made up of a an unpressurised module for propellant, water and gas, and a pressurised cargo carrier for dry cargo.
First ATV launched by Ariane 5 from Kourou on 9 March. 08. After 25 days of autonomous transfer flight (including demonstration mission), Jules Verne arrived at the International Space Station and docked automatically to rear of Russian Service Module (Zvezda) on the 3rd April 2008.
Generic ATV can carry a total cargo of up to 9 t:• up to 5.5 t of dry cargo
(re-supply goods, scientific payload, etc) • up to 840 kg of water and 100 kg gas• up to 860 kg of propellant for refuelling the Station• up to 4.7 t of propellant for ISS propulsive support (reboost, attitude control, debris avoidance manœuvre).
ATV Johannes Kepler docking
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Additional ESA-provided Elements
Data Management for Zvezda (Roskosmos) On-orbit since July 2000
Super Guppy (NASA) Delivered October 1997
Microgravity Science Glovebox (NASA)On-orbit since July 2002
Crew Refrigerator/
Freezer
(NASA) QM delivered September ’05 FM Cancelled
Node 3
(NASA) Delivered early 2007
- 80°
C Freezer (MELFI ) (NASA
and JAXA )FM 1 delivered March 2002
to fly on ULF1.1
FM 2 delivered July 2004
Cupola (NASA) Delivered September 2004
Hexapod (NASA) Storage 2005-2008
Node 2 (NASA) Delivered June 2003
European Robotic Arm
(Roskosmos) Delivery to Russia May ’06 Launch with MLM 2009
ATV Johannes Kepler docking
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ATV technical data
Kourou, French GuianaLaunch site
Electrical power will be supplied by non rechargeable batteries.
ATV will be launched with its solar panels folded to the body of the spacecraft.
Ariane 5 (260x260 km, 51.6°
transfer path)
Launch vehicle
Total net cargo upload capacity:7667 kg
ISS re-boost and attitude control propellant: 0-4500 kg
Gas (Nitrogen, Oxygen, air, 2 gasses/flight): 0-100 kg
Water: 0-840 kg
Dry cargo: 1500-5500 kgCargo mass
2 x 0.314 m3 and 2 x 0.414 m3 for each of 8 racks
Payload envelope
Launch Configuration
ATV Johannes Kepler docking
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Vehicle comparison
ATV Johannes Kepler docking
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 unpressurized)
14 m3 6.6 m3 6.17 m3
Cargo Upload Capacity 6000kg 7667kg 2230-3200kg Lunar mission
Engine Thrust 4x500N = 2000N 4x490 N = 1960N 2942 N 1x97860 N
Page 24ISS 2004-03ATV Johannes Kepler docking ATV-CC – 24th February 2011 24
Docking system
ATV Johannes Kepler docking
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Optical guidance
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Docking system probe deployment
ATV Johannes Kepler docking
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Cargoes integration and cleaning
ATV Johannes Kepler docking