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Moureaux Aurélien France Air Liquide Advanced technologies ID : 3125316 Title : NEW COMPONENT DEVELOPMENTS FOR ELECTRIC PROPULSION SYSTEMS Theme : Resume : Electric Propulsion is a major breakthrough in platform architecture, reducing dimensions and mass thus leading to different options for launchers, modifying daily operation program and orbit raising program. Electric propulsion is now used for all range of satellites, from scientific missions to telecom bus, from nano-satellites to 6 tons platforms, from one time project to constellations. Electric propulsion uses mainly xenon as propellant; other gases like krypton may also be used. Propulsion subsystems are very conservative in their way of handling propellant and delivering it to thrusters. Air Liquide Advanced Technologies has developed a high pressure gas mass flow controller which brings a new breakthrough in propulsion subsystem design. This paper presents development status and roadmap of Electric Propulsion products at Air Liquide. Powered by TCPDF (www.tcpdf.org)

Title : NEW COMPONENT DEVELOPMENTS FOR ELECTRIC … · 2016. 12. 28. · Theme : Resume : Electric Propulsion is a major breakthrough in platform architecture, ... Electric propulsion

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  • Moureaux Aurélien

    France

    Air Liquide Advanced technologies

    ID : 3125316

    Title : NEW COMPONENT DEVELOPMENTS FOR ELECTRIC PROPULSIONSYSTEMS

    Theme :

    Resume :

    Electric Propulsion is a major breakthrough in platform architecture, reducing dimensions and mass thus leading to differentoptions for launchers, modifying daily operation program and orbit raising program. Electric propulsion is now used for all rangeof satellites, from scientific missions to telecom bus, from nano-satellites to 6 tons platforms, from one time project toconstellations.Electric propulsion uses mainly xenon as propellant; other gases like krypton may also be used. Propulsion subsystems are veryconservative in their way of handling propellant and delivering it to thrusters. Air Liquide Advanced Technologies has developeda high pressure gas mass flow controller which brings a new breakthrough in propulsion subsystem design. This paper presentsdevelopment status and roadmap of Electric Propulsion products at Air Liquide.

    Powered by TCPDF (www.tcpdf.org)

  • New component for electric propulsion Space Propulsion Forum

    Roma, 05/05/2016 l Aurélien Moureaux l SPACE BUSINESS UNIT

    Advanced Technologies

  • 2 Air Liquide, world leader in gases, technologies and services for Industry and Health

    Mass flow regulation

    ■ Whatever the gas: Helium Hydrogen Oxygen Nityrogen Xenon Specific Mixtures ...

    ■ From capillary ... to DN 50

    fuite

    Chromatography

    Control

    5 g/s

    Power

    1 kg/s

    200g/s

    Pressurisation

    Keep pressure in tanks

    Launcher

    Chemical composition

    analysis

    Controlled cold massflow

    Energy flow

    30g/s

    µg/s

    20 mg/s Xenon massflow

  • 3 Air Liquide, world leader in gases, technologies and services for Industry and Health

    Ariane – Helium Pressure regulator

    ■ Pressure regulation on Ariane 5 EPS : 2 stages mechanical pressure regulator Operational temperature: de –100°C à +70°C Still in production

    ■ Developments for A5 ME & A6: Full pressurization plate: regulator/relief valve/plenum/back-flow control Operational temperature: de –120°C à +50°C Extension based on A5 EPS pressure regulator (modified mass-flow and pressure)

  • 4 Air Liquide, world leader in gases, technologies and services for Industry and Health

    Solutions – Downscale

    ■ Space products downscale

    Mass Performances Costs / Time

    Space Development

  • 5 Air Liquide, world leader in gases, technologies and services for Industry and Health

    Typical Electric Propulsion System

    ■ Pressure regulator Up to 200 bar

    ■ 4 XFC Low inlet pressure 2-3 bar Complex elements Electronically driven

    ■ +Filters ■ +Latch valves ■ +redundances...

    Complex Heavy Costly

  • 6 Air Liquide, world leader in gases, technologies and services for Industry and Health

    Thermally controlled Valve

    ■ Onboard: Rosetta ExoMars (MOMA)

    ■ Mass # 5g ■ Electric power # 2 W

    ■ Xenon / Krypton / N2 / He etc. ■ Inlet pressure: 5-200 bar ■ Temperature range: -60/+60 °C ■ Tightness < 1.10-8 mbar.l/s Ghe

  • 7 Air Liquide, world leader in gases, technologies and services for Industry and Health

    Thermally controlled Valve

    ■ Pressure Regulation Gas Chromatograph Thruster

    ■ Mass flow control Thruster

    Current driving

  • 8 Air Liquide, world leader in gases, technologies and services for Industry and Health

    Proposed architecture

    ■ No pressure regulator

    ■ 4 XFC High inlet pressure High leak tightness Electronically driven

    Simpler Lighter Cost saving

  • 9 Air Liquide, world leader in gases, technologies and services for Industry and Health

    Thermally controlled Valve

    Leakage < 10-9 Ncc/s GHe

  • 10 Air Liquide, world leader in gases, technologies and services for Industry and Health

    Thermally controlled Valve

    Mass flow as a function of valve temperature at a constant inlet pressure

  • 11 Air Liquide, world leader in gases, technologies and services for Industry and Health

    Thermally controlled Valve

    Mass flow: 0 – 20 mg/s Inlet pressure: 5-150 bar

  • 12 Air Liquide, world leader in gases, technologies and services for Industry and Health

    VanneConsigne de débit (mg/s) Courant (A)

    Fonction de transfert(TBD)

    MoteurXe avec débit régulé

    Mesure de courant de décharge (unité TBD)Débit calculé (mg/s)

    Mesure de débit (g/h He)

    Débitmètre

    Fonction de transfert(g/h He à mg/s Xe)

    High presure inlet XFC

    Mass flow command

    Transfert function

    Valve Mass flow meter

    Thruster

    0

    5

    10

    15

    20

    25

    -20 0 20 40 60 80 100 120Temps [sec]

    D1 [mg/sec Xe]

    D1 [mg/sec Xe]

    Mass flow measurement

  • 13 Air Liquide, world leader in gases, technologies and services for Industry and Health

    VanneConsigne de débit (mg/s) Courant (A)

    Fonction de transfert(TBD)

    MoteurXe avec débit régulé

    Mesure de courant de décharge (unité TBD)Débit calculé (mg/s)

    Mesure de débit (g/h He)

    Débitmètre

    Fonction de transfert(g/h He à mg/s Xe)

    High presure inlet XFC

    Discharge current

    commant

    Transfert function

    Valve Thruster

  • 14 Air Liquide, world leader in gases, technologies and services for Industry and Health

    Thermally controlled Valve

    ■ Pressure Regulator ■ Mass flow regulator

    ■ Pulse-width modulation ■ Current driving

    ■ High Pressure ■ Very good Tightness ■ Xenon / Krypton ■ Helium ■ N2

  • 15 Air Liquide, world leader in gases, technologies and services for Industry and Health

    Micro Latched Valve

    Inlet pressure 5 bar Mass < 5 grams Size 10mm x 10mm x 20mm Power 5 W Opening time < 100 ms Leakage

  • 16 Air Liquide, world leader in gases, technologies and services for Industry and Health

    Conclusion

    ■ Components qualified in Helium ■ Onboard ExoMars 2018 ■ Electronic regulation

    Any mass flow within the range ■ Examples of use:

    Gas Chromatograph Electric Propulsion Inflatable structures Cold Gas Propulsion

    ■ Firings with thrusters (2016)

  • End of presentation Thank you for your attention