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QSP  
Initial Operational Capability (IOC):
Total Production: ?
Also Known As: Quiet Supersonic Platform
Origin: United States of America
Corporations: Lockheed Martin and Northrop Grumman
Parent System: QSP
Initial Operational Capability (IOC):
Total Production: ?
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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.

QSP Specifications

Performance
Max Range: 11,112 kilometer (6,000 nautical mile)
Speed
Cruise Speed: 797 mps (2,870 kph)
Weight
Max Takeoff Weight: 45,360 kilogram (100,000 pound)
Payload: 9,100 kilogram (20,062 pound)
CEP: Circular Error Probable
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)

QSP News

There is 1 news
on 28 Aug 2003
Thursday, August 28, 2003Northrop-Grumman, DARPA and NASA Start Sonic Boom Tests

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