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Airbus Defence and Space Spaceplane

Spacecraft and Launch Vehicles

The Airbus Defence and Space Spaceplane, also called the EADS Astrium spaceplane, was a suborbital spaceplane concept for carrying space tourists, proposed by EADS Astrium, the space subsidiary that later became part of Airbus Defence and Space. A full-size mockup was unveiled in Paris on 13 June 2007. The design was a rocket plane with a large straight wing and a pair of canards, using turbofan jet engines for the atmospheric phase and a reusable methane and oxygen rocket engine for the climb to about 100 kilometres. It was to carry a pilot and four passengers and weigh about 18 tonnes at take-off. Astrium hoped to begin development in 2008 and fly in 2011, and priced a ticket at 200,000 euros,, but as of 2015 it was still waiting for investors. The mockup is now displayed at the Musée de l'Air et de l'Espace.

Facts
Propulsion
Liquid Methane 1
Engine Class
Jet 1
Engine Class
Rocket 1
Status
Design only (never built) 1
Maximum Mass (kg)
18,000 1
Comparison
Body Style
Spacecraft 1
Connections

Exemplifies

Source Airbus Defence and Space Spaceplane (Wikipedia)

Of Make

Source Airbus Defence and Space Spaceplane (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Airbus Defence and Space Spaceplane (Wikipedia)Lead
Quote, Lead
a suborbital spaceplane concept for carrying space tourists, proposed by EADS Astrium (currently Airbus Defence and Space)
Sources
1. Airbus Defence and Space Spaceplane (Wikipedia)
  • Lead
    a suborbital spaceplane concept for carrying space tourists, proposed by EADS Astrium (currently Airbus Defence and Space)
  • Lead, jet engines
    Propulsion is ensured by classical turbofan jet engines for the atmospheric phase and a methane-oxygen rocket engine for the space tourism phase.
  • Lead, rocket engine
    Propulsion is ensured by classical turbofan jet engines for the atmospheric phase and a methane-oxygen rocket engine for the space tourism phase.
  • Lead, methane propellant
    Propulsion is ensured by classical turbofan jet engines for the atmospheric phase and a methane-oxygen rocket engine for the space tourism phase.
  • Characteristics
    The total mass of the vehicle is 18 metric tons (39,700 lb) at takeoff.
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