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WBW-1/Plasma Eagle I
   
 

The Wavelev Body Wing 1/Plasma Eagle I is a Wavelev™/Raylev™ train and hence a Vertical Take-Off and Landing (VTOL) aerial vehic- le.
The Plasma Eagle I has its name from the direct integration of the propulsion and lift system of the Lightcraft by the Rensselaer Poly- technic Institute and our MagnetoAir-PlasmaJet (MAPJ), and our aircraft model BWB-1/White Eagle with its Blended Wing Body (BWB).

Interior
Basically, the WBW-1/Plasma Eagle I features the same interior like our BWB-1/White Eagle.

Images

NASA N3-X with Superconducting Electric Motors and Turbine based Power Generator (Image by NASA)
Leik N. Myrabo with Rensselaer Polytechnic Institute→Lightcraft Ion Propulsion and Ionized Plasma Propulsion with MHD Slipstream → OntoLab and Style of Speed Raylev Transport System→WBW-1/Plasma Eagle (Image Rensselaer Polytechnic Institute)Leik N. Myrabo with Rensselaer Polytechnic Institute→Microwave Lightcraft Ion Propulsion and Ionized Plasma Propulsion with MHD Slipstream → OntoLab and Style of Speed Raylev Transport System→WBW-1/Plasma Eagle (Image Rensselaer Polytechnic Institute)

Specification

  • Concept: Style of Speed
  • Design Exterior: NASA, Rensselaer Polytechnic Institute, and Style of Speed
  • Design Interior: Style of Speed and partners
  • Powertrain: Raylev™/Wavelev™ with beamed energy system, elec- tric MagnetoAir-PlasmaJet (MAPJ), and fuel cell or turbine based emergency power generator
  • Steering: Classic mechanical, drive-by-wire or drive-by-light, fly-by-wire or fly-by-light, or combinations
  • Active component™ option: MagnetoHydroDynamics (MHD) slipstream accelerator, Active Anti-Friction, and Active Aerodynamics
  • Option: In-wheel electric motor
  • Seats: 200 up to 400

    Further Informations
    The Plasma Eagle I can land on every area that has the size of a football field.

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