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2016 ESA/NASA 2016 ESA/NASA

2016 ESA/NASA - PowerPoint Presentation

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2016 ESA/NASA - PPT Presentation

ExoMars Trace Gas Orbiter Mark Allen Jet Propulsion LaboratoryCalifornia Institute of Technology Olivier Witasse European Space Agency 1 Copyright 2011 All rights reserved Artists concept ID: 462290

purposes decisional planning discussion decisional purposes discussion planning pre science esa relay 2016 amp moi phase edm launch orbit

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Slide1

2016 ESA/NASA ExoMars/Trace Gas Orbiter

Mark AllenJet Propulsion Laboratory,CaliforniaInstitute of TechnologyOlivier WitasseEuropean Space Agency

1

Copyright 2011. All rights reserved.

Artist’s concept

MEPAGJune 16, 2011

Pre-decisional – for planning and discussion purposes onlySlide2

Joint ESA-NASA Mars OrbiterProposed launch in 2016Deliver ESA EDM

1 Mars year orbital science missionTelecom asset until 2022Overview2Slide3

Contributions

HISCI

NASA / JPL

Proposed

Mission

ElementsElectra

Atlas-V

– Baseline

431

Class

JPL SRA

JPL DSN

EMCS

MAGIE

MATMOS

ESA Mission Elements

ESA ESOC

Entry / Descent Module (EDM)

ESA ESTRACK

NOMAD Inst.

Spacecraft / Orbiter

3

Pre-decisional – for planning and discussion purposes onlySlide4

EMTGO Mission Events (proposed)

4

EDM release at MOI - 3 days

Orbiter retargets to MOI altitude

MOI captures to 4 sol orbit

Atlas V 431

LAUNCH

INTERPLANETARY

CRUISE

APPROACH, EDM RELEASE

& MOI

Jan 2016

EMTGO in launch

configuration

EDM RELAY & TRANSITION

TO 1-SOL ORBIT

Launch

Jan 2016

Arrival

Oct 2016

November 2016 to June 2017

Type II Trajectory: C3 = 7.44 km

2

/s

2

Science Phase: 1 Mars Year 6-2017 to 6-2019

Relay Phase: 2018 Rovers Jan 2019

Relay Phase: Future Missions through 2022

MOI &

EDL

Comm

4-sol

orbit

1-sol

orbit

AEROBRAKING PHASE

7 month

Aerobraking

SCIENCE & DATA RELAY

PHASE

Science & Relay Orbit

400 km Frozen

Rotates every

4 months

Phased for 2018 Relay

Transition to

Science Orbit

DSM

May 2016

EDM Relay provided

by NASA Relay Orbiters

Change Inclination for Science Orbit

Pre-decisional – for planning and discussion purposes onlySlide5

Prioritized Science Objectives

Detect a broad suite of atmospheric trace gases and key isotopologues.

Characterize the spatial and temporal variation of methane and other species that could be signatures of active biological and/or geological processes (for example, C2

H6, SO

2, N2

O) and of photochemical species that determine atmospheric lifetimes (e.g., representative Ox, HOx, NOx species) and their source molecules (e.g., H2O).

Localize the sources and derive the evolution of methane and other key species and their possible interactions, including interactions with atmospheric aerosols and how they are affected by the atmospheric state (temperature and distribution of major source gases; e.g. H

2

O).

Image surface features possibly related to trace gas sources and sinks.

5

Pre-decisional – for planning and discussion purposes onlySlide6

Proposed Payload

6

MATMOS

Solar occultation Fourier transform IR spectrometer

(w/ Canadian contribution)

NOMAD

Occultation + mapping IR, Vis, UV spectrometer

(consortium of Belgium, Spain, Italy, UK)

EMCS

Thermal IR spectrometer

MAGIE

Wide-angle Vis-UV camera

HiSCI

High resolution, colour, stereo camera

(w/ Swiss contribution)

nadir

Pre-decisional – for planning and discussion purposes onlySlide7

Ultrahigh sensitivityBright light sourceLong

pathlengthOrbit inclination: 74ºSolar occultation7

Pre-decisional – for planning and discussion purposes only

Spring

SpringSlide8

Ground track for 3 days

Nadir mapping8Pre-decisional – for planning and discussion purposes only