Workshop on European Space Information Technology in the 21st Century Future Mission Needs for Infor - PowerPoint PPT Presentation

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Workshop on European Space Information Technology in the 21st Century Future Mission Needs for Infor

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Magnetometer - Ion Spectrometer - Electron Analyser - Cold Plasma Analyser ... Magnetometer - Alpha X-ray spectrometer - Subsurface detectors - Mole - Micro-rover ... – PowerPoint PPT presentation

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Title: Workshop on European Space Information Technology in the 21st Century Future Mission Needs for Infor


1
Workshop on European Space Information
Technology in the 21st CenturyFuture Mission
Needs for Information TechnologyScience
Missions
  • 27 - 28 September 2000, ESOC, Darmstadt, Germany
  • Giorgio Bagnasco, ESA D/SCI
  • Future Project Studies Technology Office

2
ESA D/SCI Program Horizon 2000
3
The Mercury Planetary Orbiter
Main Mission Objective - Remote Sensing -
Radio Science Mass 360 kg Power 420W Data Rate
up to 350 kbits / sec Lifetime gt 1
year Candidate Payload Suite - Visible
Cameras - IR,UV, X, ?, Neutron Spectrometers -
Laser Altimeter
4
The Mercury Magnetospheric Orbiter
Main Mission Objective - Fields Particles
Science Mass 160 kg Power 185 W Data Rate up
to 40 kbits / sec Lifetime gt 1 year Candidate
Payload Suite - Magnetometer - Ion
Spectrometer - Electron Analyser - Cold Plasma
Analyser - Energetic Plasma Detector - Visible
Camera
5
The Mercury Surface Element
Mission Objective - Surface Chemical /
Physical Properties Mass 44 kg Energy 1700 W
h Data Rate up to 9 kbits / sec Lifetime gt 1
week Candidate Payload Suite - Cameras -
Seismometer - Magnetometer - Alpha X-ray
spectrometer - Subsurface detectors - Mole -
Micro-rover
6
GAIA
Mission Objective - Global Astrometry - Radial
Velocity Spectrometry - Photometry Mass 3140
kg Power 2570 W Data rate8 Mbit / sec (for 8
hr/day) Lifetime 5 year Orbit L2 Candidate
Payload - 2 identical SiC telescopes for
astrometry - 1 telescope for spectrometry
photometry
7
IRSI-Darwin
Mission Objective - Detection of Earth-like
planets Mass ?3500 kg Power ? 1650 WData Rate ?
20 kbits / sec Operating wavelength 5-18 ?m
Orbit L2 point Lifetime 5 years
8
Objective Gravitational wave detection Mass 3
x 400 kg Power 1300 W Baseline 5 x 106 km Orbit
60 deg inclined, Sun orbit at 1AU Data Rate 7
kbits/ sec Lifetime 2 years
9
XEUS
Mission Objective - Cosmology by X-ray
Spectroscopy Mass (6000 25000) kg Power
(12000 1000) W Orbit Low Earth Orbit (600
km) Data Rate 100 kbit / sec Lifetime gt 25 years
10
Review of the D/SCI Technology Development
Activities
  • Overall Objectives Benefits
  • Harmonic D/SCI Technology Programme
  • Development of technologies for D/SCI Future
    Missions within schedule and budget
  • Overview of all the schedules for Technology
    Activities and related costs
  • Provision of rationale to the "External World" of
    D/SCI plans and priorities
  • Possibility to improve synergy with other
    Directorates
  • Risk Reduction for D/SCI Future Missions

11
D/SCI Technology Development Activities
12
CS 5 Nominal Schedule
13
D/SCI Technology Development Activities
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