09.12.2014. Turin. ALTEC.

ExoMars Progress Report

ExoMars Science Working Team

09-12-2014

ExoMars Progress Report

ExoMars Science Working Team

09-12-2014

09.12.2014. Turin. ALTEC.

ESA ESTRACK

2016 Mission

Carrier Module (CM)

Surface Platform

NASA DSN

Rover

Descent Module (DM)

2

SchiaparelliEDL Demonstrator Module (EDM)

MOCC @ ESOC Spacecraft Operations

Science Operations Centre ESAC

ROS Antennas

ROCC

Science Archive Back-up Centre IKI

LPOCC

Programme OverviewTwo missions launched in 2016 and 2018 The 2016 mission consists of a Trace Gas Orbiter (TGO) and an EDL Demonstrator Module (EDM)

The 2018 mission consists of a Carrier Module (CM) and a Descent Module (DM) with a Rover and a stationary Landing Platform

Trace Gas Orbiter (TGO)

Proton M

2018 Mission.

Proton M

09.12.2014. Turin. ALTEC. 3

Main Organisation Documents & ActivityDocument & activity Status

Cooperation Agreement Signed

Joint Management Plan Signed

2018 mission Responsibility Matrix Signed in 2013 and 2014 (update)

2016 mission Responsibility Matrix Signed in 2014

Planning Agreement Signed in 2013 and 2014

(update)

2016 and 2018 missions Master Schedules Under revision

Joint Configuration Control Management Document Signed

ExoMars Joint Programme Objectives Document Signed

Joint ExoMars Steering Board Formed

Chief Designers‘ Board Formed

Standards Review Working Group Formed and operational

Landing Site Selection Working Group Formed and operational

09.12.2014. Turin. ALTEC. 4

TGO Science Instruments.

ACS – Atmospheric Chemistry Suite. The three spectrometers cover respectively the bands 0.7–1.7 µm, 2.3–4.6 µm., and 1.7–17.0 µm. ACS will study trace gases, profile isotope ratios, and contribute to atmospheric escape studies.

Status: ACS-STM delivered to TAS-F. Flight hardware is scheduled for delivery at the end of March 2015.

FREND - Fine Resolution Epithermal Neutron DetectorNeutron detector with a collimation module to significantly narrow the instrument’s field of view, thus allowing the creation of higher resolution maps of hydrogen distribution.

Status: FREND-QM delivered to TAS-F. Flight hardware is scheduled for delivery at the end of February 2015.

09.12.2014. Turin. ALTEC. 5

Progress on the 2018 Mission

MISSION & SYSTEM Joint DM Design Review

2018 DM DR Board Close-out took place on 13 October 2014

Several issues remained open however it was agreed to forward the open RIDs and issues to the S-PDR panels for disposition

System PDR S-PDR Board session was held on November 6, 2014, with equal co-chairing of the

European and the Russian participants

After the session the conclusion was made that S-PDR objectives has not been fully achieved

Final session of S-PDR Board is planned on May 5, 2015.

March 2015March 2015 May 2015May 2015April 2015April 2015February 2015February 2015December 2014December 2014 January 2014January 2014

Actions ClosureActions Closure Actions

Acceptance #1Actions

Acceptance #1

ActionsAcceptance #2

2

ActionsAcceptance #2

2

ResponsibilityMatrix Draft

ResponsibilityMatrix Draft

Close-Out Package Delivery

Close-Out Package Delivery Co-locationCo-location

Panel Endorsement

Panel Endorsement S-PDR CO BoardS-PDR CO Board

09.12.2014. Turin. ALTEC. 6

Progress on the 2018 Mission

DESCENT MODULE The DM baseline configuration is updated based on the DM DR outcome

DM de-scoping re-distribution of functions of the Russian OBC-2 between the other Russian Units and

European OBC-1

decrease of mass of the European RM decrease of mass of the Russian scientific equipment on Landing Platform

Increase of clearance of landing platform Optimization of power supply/ power consumption system

It is necessary to finalize PAS baseline configuration (number of stages, number of fixation points, loads at deployment etc.)

CARRIER MODULE A Carrier Module Design Review (Industry Level Review) completed

It is necessary to solve the issues on Power Supply System, thruster impact on DM, avoidance of collision with DM after separation

09.12.2014. Turin. ALTEC.

Descent Module (DM)

2018 SCC Overview – Cruise Configuration

Adapter with separation system

Carrier Module (CM)

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Parachute system

Back Shield

Rover

2018 DM Configuration

Lander

Front Shield

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Rover

Landed Platform with Rover – latest configuration

Lander

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Milestone Date

ESA Council at Min. Level 2 December 2014.

2016 FM FREND and ACS deliveries to ESA February – March 2015

2018 Mission CD/E1 Rider 2 signature 1 April 2015

2018 Mission C/D Kick-Off TBD

2018 Mission S-PDR CO Board 4 May 2015

2016 Mission SCC Adaptor and Separation Mechanism Test

June 2015

2016 Mission EDM/TGO Mating for SCC Test 11 June 2015

2016 Mission FAR September 2015 (TBC)

2016 Missions start Launch Campaign in Baikonur 26 October 2015

Major Short TermMilestones