RS-88  
Initial Operational Capability (IOC): 2005
Total Production: ?
Origin: United States of America
Corporations: Boeing
Parent System: RS-88
Initial Operational Capability (IOC): 2005
Total Production: ?
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Description: The RS-88 is a 50,000-pound thrust class rocket engine designed by Boeing for use on Lockheed-Martin's Pad Abort Demonstration (PAD) vehicle to be launched in late 2005. PAD is a program sponsored by NASA and will be powered by 4 RS-88 rocket engines.

RS-88 Specifications

Weight
Thrust: 50,000 pound (22.7 ton)
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)

Operators & Related Equipment


OperatorsItems

Grand Total ?1
 
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