YF-115

YF-115

Country of origin	China
First flight	2015-09-20
Designer	Academy of Aerospace Liquid Propulsion Technology
Associated L/V	Long March 6 and Long March 7
Status	In service
Liquid-fuel engine
Propellant	LOX / RP-1
Mixture ratio	2.5
Cycle	Oxidizer-rich Staged combustion
Configuration
Chamber	1
Performance
Thrust (vac.)	176.5 kN (39,700 lbf)
Thrust (SL)	147.1 kN (33,100 lbf)
Chamber pressure	12 MPa (1,700 psi)
Isp (vac.)	341.5 seconds (3.349 km/s)
Dimensions
Length	2,325 millimetres (91.5 in)
Diameter	946 millimetres (37.2 in)
Used in
Long March 6 second stage and Long March 7 second stage.

The YF-115 is a Chinese liquid rocket engine burning LOX and kerosene in an oxidizer-rich staged combustion cycle. A high efficiency/high thrust environmental friendly rocket engine was always an objective within Programme 863. But the Chinese industry was not mature enough to produce such a rocket until they obtained examples (and probably documentation) of the Russian RD-120 in the early 1990. Development began in the 2000s, along with its sibling, the bigger YF-100, which would power the LM-5, LM-6 and LM-7 boosters and first stages. Testing was directed by the China National Space Administration (CNSA) commencing in 2005. Development works are mainly carried out by the Xi'an Aerospace Propulsion Institute. It will be used as upper stage engine for China's next generation of medium and light environmental-friendly launch vehicles, namely the Long March 6 and the Long March 7. During early 2012, the engine system successfully passed vacuum testing. It is China's first upper stage rocket engine to adopt the staged-combustion cycle.

In the LM-6 upper stage it will use a single YF-115 with gimbaled mount. While the LM-7 upper stage will use four such engines. But in this latter case, two engines will be fixed and two will be gimbaled.