VENµS MISSION STATUS VENµS users meeting – Jan 2010 Pierric FERRIER, CNES.

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VENµS MISSION STATUS VENµS users meeting – Jan 2010 Pierric FERRIER, CNES

Transcript of VENµS MISSION STATUS VENµS users meeting – Jan 2010 Pierric FERRIER, CNES.

Page 1: VENµS MISSION STATUS VENµS users meeting – Jan 2010 Pierric FERRIER, CNES.

VENµS MISSION STATUS

VENµS users meeting – Jan 2010Pierric FERRIER, CNES

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1- Camera status

2- Bus status

3- Ground segment status

4- Launcher status

5- Summary

Content

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CEU

DETECTORSASSEMBLY

BEZEL

TUBE

SUNSHIELD

THERMAL CONTROLSHIELD

SMA PMA CORRECTIONLENSES

Camera longitudinal section

1- Camera status

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Tube equipped with both mirrors

1- Camera status

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Correction lens assembly

1- Camera status

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Thermal control shield (external cylinder)

1- Camera status

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Camera status synthesis

~1.4 mm 2.0 mm

8.0 mm 10 mm

Blocking Filter

Narrow-band Filters

1- Camera status

BARR filters= the weakest link of the chain, so far...

•18 months needed to obtain the ITAR approval

•13 months delay in manufacturing due to technical issues (delivery expected in March)

The current schedule shows a camera delivery at end of Aug 2011

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-Mass: 250kg -Power: 800w

-Overall stowed dim: 1.6x1.2 m

-2xSTR - 2 X-band - 1xIHET redunded , 16 Kg Xenon - 4x1N redunded thrusters, 7 Kg hydrazine

2– Bus status

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2– Bus status

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2– Bus status

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2– Bus status

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Bus status synthesis

2– Bus status

• Base plate to be delivered this quarter (from RAFAEL to IAI)

• Other parts of the bus are stored and ready for final bus assembly (solar pannel, satellites pannels - 6 of them, and all bus internal subsystems)

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SMIGSIsraeli Ground Control Station

GCS

Israeli Technological Mission

Ground CenterTMC

IHET Telemetry

ProgrammingMessages

Catalogue&

Products

VENµSProducts Distribution

DownloadMessages

& Image TM

S band

X band

VENµS Image Qualityunit

VENµS scientific mission programing & Image Processing

unit

Browsing

& Products by network

KIRUNAX Band Receiving

Station

Scientific mission FRANCE

Satellite command & control and technological mission ISRAEL

3– Ground segment status

Ready end of 2010 Ready end of

2010

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4– Launcher status

The foreseen launcher for Venµs is PSLV so far.

Unfortunately this scenario faces 2 issues • at the INDIAN government level• as Venµs would be the co-passenger, the risk exist to be injected in a non optimal orbit (i.e. 666 km – 3days instead of 720 km -2 days)

•Nevertheless, other scenarios exist, the main one being a launch with PLEIADES 2 on SOYOUZ

•Current engineering practice calls for a final launcher selection 2 years ahead of the foreseen launch date. In other words the launcher will be selected in 2010.

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Mission timeline

last quarter

2009 2011

CAMERA

MISSION GROUND SEGMENT

IHET

SATELLITE

GROUND CONTROL SEGMENT

2012 2015

mid year

MISSION

……

5- Summary

2010