Designed and developed by China Academy of Launch Vehicle Technology (CALT), 'Long March 5' ('LM-5', 'CZ-5', or 'Changzheng 5') is China's next generation space launch vehicle family, which would include a range of classes of launch vehicles for different missions.
Development
Early reports stated that the CZ-5 project was announced in February
2001, with the initial development officially beginning in
2002. China hoped that the CZ-5 would fulfill the requirement for large payload
LEO and
GEO missions for the next 20–30 years, with the first versions of the vehicle going into service by
2008. Chief Designer for the CZ-5 was
Long Lehao.
However, a new report on
November 3,
2005, said that according to Wu Yansheng at the China Academy of Launch Vehicle Technology, the CZ-5 was still awaiting final approval and would take about six years for development, being ready in
2012.
[1] A further report on
November 27,
2005, quoted the deputy commander of the manned space program saying that CZ-5 was still waiting for funding approval.
Design
According to reports, the CZ-5 family will include three primary modular core stages of 2.25 m, 3.35 m and 5.0 m diameter. Boosters of various capabilities would be assembled from three modular core stages and strap-on stages. There would be a choice of engines with different
liquid rocket propellants: 1,200 kN thrust
LOX/
kerosene engines or 500 kN thrust LOX/
LH2 engines on first stage and boosters. The upper stage would use improved version of
YF-75 engines.
Engine development began in 2000-2001, with testing directed by the China National Space Administration (CNSA) commencing in 2005. Versions of both new engines:
YF-100 and
YF-77 had been successfully tested by mid-2007.
The CZ-5 series will deliver 1.5
t to 25 t payload to LEO, or 1.5 t to 14 t payload to GTO (geosynchronous transfer orbit). This would replace the CZ-2, CZ-3, and CZ-4 series in service, as well as providing new capabilities which are not possessed by the current
CZ family. The heaviest configuration of the CZ-5 with a 5.0 m diameter core stage and four 3.35 m diameter strap-on boosters should be able to send a 25 t payload to low earth orbit.
'Comparable rockets:'
Delta IV Heavy -
Atlas V -
Ariane 5 -
Angara A5 -
Proton -
Falcon 9 -
GSLV III
References
http://www.geocities.com/launchreport/cz5.html