SALACIA SAline Liquids And Conductivity In the Atmosphere A REXUS - - PowerPoint PPT Presentation

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SALACIA SAline Liquids And Conductivity In the Atmosphere A REXUS - - PowerPoint PPT Presentation

SALACIA SAline Liquids And Conductivity In the Atmosphere A REXUS project Presented by: Daniel Nilsson Lule University of Technology, Kiruna, Sweden www.salacia.se 1 Outline The REXUS/BEXUS program Scientific background The


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SALACIA

SAline Liquids And Conductivity In the Atmosphere A REXUS project

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Presented by: Daniel Nilsson Luleå University of Technology, Kiruna, Sweden www.salacia.se

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Outline

  • The REXUS/BEXUS program
  • Scientific background
  • The SALACIA mission
  • Discussion

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The REXUS/BEXUS program

“The REXUS/BEXUS programme is realized under a bilateral Agency Agreement between the German Aerospace Center (DLR) and the Swedish National Space Board (SNSB). The Swedish share of the payload has been made available to students from other European countries through a collaboration with the European Space Agency (ESA).”1

  • 1. www.rexusbexus.net

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REXUS timeline

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  • 18 m

Call for proposals

  • 15.5 m

ESTEC workshop

  • 15 m

Final selection

  • 8.5 m

Student Training Week

  • 4 m

Integration week + 0 Launch

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Scientific Background

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Credits: Martin-Torres & Zorzano
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Scientific Background

time

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Credits: Martin-Torres & Zorzano
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The SALACIA mission

Salt behavior and conductivity

■ under stress ■ low pressure ■ low Relative Humidities (RH) ■ different temperatures

Designing an instrument to study perchlorates (on Mars and Earth)

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Experiment Design

Layout view for SALACIA experiment

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Mechanical structure

5 vessels, each have a volume of ~9000 mm3 Cylindrical shape of the vessels (not yet determined), mass below 2kg Take advantage of counterclockwise spin

Current preliminary design

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Old design

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Electrical structure

  • 1 microcontroller unit with a power consumption of about 20mA-

50mA

  • 1 power supply unit with an estimated power dissipation of ~37 mA
  • Conductivity sensors are estimated to consume, at worst case ~200

mA

  • Heating with power resistor of 100 Ohm, power consumption of 0.3

A, (10W)

  • The total current drawn, with a 20% adding to the MCU and PSU, is

estimated to be ~76 mAh (if the time of flight is ~800 seconds)

  • The camera system will have its own battery

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Expected results

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Credits: Martin-Torres & Zorzano
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The SALACIA Team

16 members Studying space technology in Kiruna, Sweden Supported by Luleå University of Technology

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Discussion

  • Post-flight examination
  • Conductivity measurements
  • Oxidizing salts
  • Laminar flow

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Thank you !

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Read more at: www.salacia.se

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Additional Slides

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Motivation

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