ChangZheng 6  
Initial Operational Capability (IOC): 2012
Maiden Flight: 2011
Total Production: ?
Also Known As: CZ-6 and Long March 6
Origin: China
Corporations: CALT
Parent System: ChangZheng 6
Initial Operational Capability (IOC): 2012
Maiden Flight: 2011
Total Production: ?
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Description: The ChangZheng 6, also known as CZ-6 or Long March 6 in the West, is a small liquid propellant space launch vehicle developed by China Academy of Launch Vehicle Technology (CALT) to place small payloads into Sun Synchronous Orbit (SSO). It is based on the 2.25-meter diameter strap-on booster developed for the ChangZheng 5 heavy space launch vehicle family. It is powered by one YF-100 engine burning Liquid Oxygen (LOX)/Kerosene propellant. The first launch is scheduled for 2010/2011.

ChangZheng 6 Specifications

Dimensions
Rocket Diameter: 2.25 meter
Weight
Payload to SSO: 500 kilogram
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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