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Intermediate eXperimental Vehicle

Suborbital Launch Vehicle

The Intermediate eXperimental Vehicle, usually called IXV, was a European Space Agency lifting-body re-entry experiment meant to validate technologies for future European reusable launchers. The craft was about 5 m long, 1.5 m high and 2.2 m wide, with a total mass of 1844 kg, and its shape was chosen to maximise internal volume for experiments. Thales Alenia Space of Torino was its contractor. It was launched on a Vega rocket from Kourou, French Guiana, on 11 February 2015 on a suborbital path of roughly 76 km by 416 km. The planned profile began formal re-entry about 120 km up at 7700 m/s, steered by moving aerodynamic surfaces and thrusters down to Mach 2, then used parachutes and airbags for a soft landing in the Pacific Ocean. Its three project objectives were re-entry system demonstration, technology experimentation and technology validation. The flight lasted only a few hours and validated a number of re-entry technologies in flight.

Facts
Status
Status (category)
Mission Complete / Ended 1
Launch Date
2015-02-11 1
Connections

Operated By

Source IXV (Gunter's Space Page)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source IXV (Gunter's Space Page)Contractors field
Quote, Contractors field
Thales Alenia Space, Torino
Sources
1. IXV (Gunter's Space Page)
  • Launch table, date
    11.02.2015
  • Description
    The IXV validated in-flight a number of re-rentry technologies, with a flight in February 2015.
  • Contractors field
    Thales Alenia Space, Torino
  • Operated By: European Space Agency, Operator field
    IXV [ESA]
  • In Group: Experimental Spaceplane and Lifting-Body Test Vehicles, Lead paragraph
    IXV is a lifting reentry body, with its shape resulting from the set of design
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