Head of ATV Mission Operations February 2011...

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

Page 2ISS 2004-03ATV Johannes Kepler docking ATV-CC – 24th February 2011 2

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


ISS today



The International Space Station

ESA-COLOMBUS

JAPANUSA

CANADA

RUSSIAESA-ATV



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


Automated Transfer Vehicle (ATV) ‏



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) ‏


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


Page 9ISS 2004-03ATV Johannes Kepler docking ATV-CC – 24th February 2011


Mission Overview

TsUP/Korolev –

24th

February 2011ATV Johannes Kepler docking


ATV Mission altitude profile



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



- 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


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 to ISS propulsive support



Automated Transfer Vehicle Johannes Kepler performances


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


Automated Transfer Vehicle Johannes Kepler Cargoes


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) ‏


ATV de-orbit and re-entry



Back –up slides


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).



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 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



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 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


Docking system



Optical guidance


Docking system probe deployment



Cargoes integration and cleaning


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Head of ATV Mission Operations February 2011...

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