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#plasmathruster β€” Public Fediverse posts

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  1. Liquid and solid propellant πŸ”₯ #rocket engines feature low mass efficiency due to the thermodynamic limitations and extremely low efficiency at small thrust. The electric πŸ”‹ thrusters do not pose limits on the propellant exhaust velocity and the propellant mass consumption may be very low nature.com/articles/s41467-017

    #ElectricPropulsion #PlasmaThruster #IonThruster #HallThruster

  2. Liquid and solid propellant πŸ”₯ #rocket engines feature low mass efficiency due to the thermodynamic limitations and extremely low efficiency at small thrust. The electric πŸ”‹ thrusters do not pose limits on the propellant exhaust velocity and the propellant mass consumption may be very low nature.com/articles/s41467-017

    #ElectricPropulsion #PlasmaThruster #IonThruster #HallThruster

  3. Liquid and solid propellant πŸ”₯ #rocket engines feature low mass efficiency due to the thermodynamic limitations and extremely low efficiency at small thrust. The electric πŸ”‹ thrusters do not pose limits on the propellant exhaust velocity and the propellant mass consumption may be very low nature.com/articles/s41467-017

    #ElectricPropulsion #PlasmaThruster #IonThruster #HallThruster

  4. Liquid and solid propellant πŸ”₯ #rocket engines feature low mass efficiency due to the thermodynamic limitations and extremely low efficiency at small thrust. The electric πŸ”‹ thrusters do not pose limits on the propellant exhaust velocity and the propellant mass consumption may be very low nature.com/articles/s41467-017

    #ElectricPropulsion #PlasmaThruster #IonThruster #HallThruster

  5. Liquid and solid propellant πŸ”₯ #rocket engines feature low mass efficiency due to the thermodynamic limitations and extremely low efficiency at small thrust. The electric πŸ”‹ thrusters do not pose limits on the propellant exhaust velocity and the propellant mass consumption may be very low nature.com/articles/s41467-017

    #ElectricPropulsion #PlasmaThruster #IonThruster #HallThruster