1_atv presentation on cargo processing

8/7/2019 1_ATV Presentation on Cargo Processing

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ESTEC 12 february 2004D. SIRUGUET MSM-EAP

ATV Ground Processing Team Slide Nr 1

ATV Jules Verne

Ground Processing

Cargo Physical Integration atKOUROU





ATV Jules Verne

Ground Processing

• Cargo Process

• Cargo Physical integration at S5C

• Cargo Late Access at BAF





ESAContainer of CTB

NASAContainer of CTB

Arrival at

Rochambeau airport

NASA responsible ESA responsible

Transportation to Rochambeaufrom cargo packing facilities

Transportation to Rochambeaufrom cargo packing facilities

CTB containers unload from commercial passenger aircraftand support for customs process

(supervised by NASA/ESA TPOC)

CTB containers transfer from Rochambeau to S5 storage area

using covered truck

(supervised by NASA/ESA TPOC)

CTB containers opening in S5airlock and transfer into ICC

ARIANESPACE responsibleUnder launch contract

Normal process of work

under ground processingmanagement

Transport coordinationby ESA

Ground processing team

Cargo Process





EPCU 3 - S5

S5AFILLING HALL

S5CPREPARATION HIGH BAY(S)

S5BINTEGRATION

&FILLING HALL

S5OFFICES

& OCOE ROOMSS5

TRANSFER CORRIDORS

A - 3





A - 7.2

EPCU 3 – S5

• Dry cargo are packed in CTBs

• CTBs are protected by pink poly plastic bags

• CTBs are stored in dedicated containers or boxes

Part of Expected documentation for receiving operations

•Lists of the content of each container (CTBs identificationn°)•Content of the CTBs of which the handle can be dangerousfor the people or the material

Dry cargo transport configuration





A - 7.2

EPCU 3 – S5





Cargo physical integration at S5C

ATV configuration for cargo integration

•ICC is on its container base in horizontal position

•The REPA ID (Racks Equipment Payload & AAC Integration Device) is

correctly positioned

•The internal floor is

installed






•Necessary documentation : Cargo map






A

AC

clos

ure

ATV

Integ

ration

Possible Dry Cargointegration

• Additional sequence:– AAC door opening

– Internal floor set-up

– cargo introduction

– internal floor removal & AAC door closure

– AAC leak test

• Following ops :– ADB, ICC CoG,..

Impact on Launch

L - 54 days (8 weeks) L - 49 days (7 weeks) Up to L - 41daysContingency case

Nominal Dry Cargo integration

• Duration: 2 days in 2 shifts (ie.1 day = 2 x 8 hours)

Possible Dry Cargo integration beforeAAC closure

Impact on Launch: max 3 days

depending on:

•overall unloading / loading duration

• Possibility of same times operations(bake out, prep. RFS & PM leak test, airrenewall, sampling,..)





BAF - Late Access





BAF - Late Access – RDS opening





BAF - Late Access – dry cargo



ESTEC 12 february 2004D. SIRUGUET MSM-EAP ATV Ground Processing Team Slide Nr 13

BAF - Late Access – RDS closure




Cargo physical integration at BAF

Late Access

„Nominal“ Late Access

• Duration: 1 day in 2shifts (ie. 1 day = 2 x8 hours)

L - 6 days L - 5days

Fairing

mating

Transfe

rtoLau

nchPa d

Up to L - 1day

Degraded Late Access if mandatory

• Additional sequence:

– Disarming & fairing removal

– Late Access Cargo integration

– Back to „nominal“ sequence

Impact on Launch:

depending on:

• launcher authorities approval

Contingency case




Launch pad

STFO switch in ZL3

Payload checks after STFO switch

Payload Battery Charge Slots0h 4h 8h 12h 16h 20h 24h

Launch Vehicle Transfer to Launch Pad

D 0D - 1

1_atv presentation on cargo processing

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