Monday, October 06, 2008

deagel.com

QSP




Origin:United States of America

Contractor/s: Lockheed Martin, Northrop Grumman

Description: The QSP (Quiet Supersonic Platform) program seeks a new technological approach for a long-range, supersonic military aircraft. This program, currently in the phase II, emphasizes on reduced sonic boom associated with the supersonic flight.

The Lockheed-Martin and the Northrop-Grumman corporations are separately developing concepts for the QSP program managed by the DARPA.

The QSP program objective is to field a supersonic vehicle with an initial shock pressure rise of no greater than 0.3 pound per square foot (1.46 kg per square meter). A typical supersonic aircraft has an initial shock pressure rise of 3 pound per square foot. The final QSP vehicle would weigh at the take-off about 100,000 pounds with a payload of 20,000 pounds, a cruise speed between Mach 2.0 and 2.4, and an unrefueled range of 6,000 nm.

Specifications
Weights: Max Weight 45,360 kg (100,000 lb), Payload 9,100 kg (20,062 lb)

Performance: Cruise Speed 797 mps (Mach 2.40), Max Range 11,112 km (6,000 nm)

News

 


Image Gallery


Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)


Last Updated: Sunday, September 28, 2008

Leave Feedback >>