March 10, 2010
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Core Competencies
.: Emerging Technologies
.: Conceptual Design
.: Analysis
.: Design
.: Manufacturing

The XP Vehicle
.: Spec & Description
.: Mission Profile
.: System Definitions
.: Technical Publications

Model XP Mission Profile

  • Takeoff Method: TurboJet Powered Horizontal Takeoff
  • Altitude at Rocket Ignition: Between 18,000 and 30,000 feet
  • Orientation at Ignition: Horizontal
  • Maximum g Force on Ascent: 3 to 4 G
  • Altitude at Rocket Engine Cut-off: 150,000 feet
  • Time at Engine Cut-off: 70 seconds
  • Maximum Speed: Mach 3.5
  • Minimum Apogee: 330,000 feet
  • Sensation of Weightlessness: 3-4 minutes
  • Reentry Method: Ballistic descent
  • Maximum g Force on Descent: 3 to 4 G
  • Landing Method: Unpowered, Horizontal Landing
  • Total Duration: < 1 hour
  • Landing Distance from Take-off Location: 0 kilometers
  • Time Between Missions: 3 to 5 days
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