TH-11
Space Pioneer (Tianbing Technology)
The TH-11 is an oxygen-rich staged combustion high-performance engine, using liquid oxygen/kerosene propellant, suitable for the upper stage and first stage of medium-sized liquid launch vehicles.
Typed specifications4 values
Discloses 2 of 10 fields engineers filter by in this category (category median 3).
- Specific impulse
- 345 s product page
- Propellant
- oxygen product page kerosene (RP-1)
- Number of starts or pulses
- 30 min · product page
Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.
As published by the supplier9 lines, in the manufacturer's own wording
- Propellant
- Liquid Oxygen + Kerosene
- Vacuum thrust
- 30 t
- Vacuum specific impulse
- 345 s
- Thrust-to-weight ratio
- 130
- Number of starts
- 2 times
- System
- Oxygen-rich staged combustion closed cycle
- Gimbaling method
- Pump-fed gimbaling
- Variable thrust range
- 50% ~ 110%
- Reusable times
- ≥30
About
The TH-11 is part of the Tianhuo series of liquid rocket engines developed by Space Pioneer (Tianbing Technology). It is an oxygen-rich staged combustion high-performance engine that utilizes liquid oxygen and kerosene as propellants. This engine is designed for use in both the upper stage and first stage of medium-sized liquid launch vehicles. Key features include a vacuum thrust of 30 tons and a vacuum specific impulse of 345 seconds. The engine boasts a thrust-to-weight ratio of 130 and can be started 2 times. It operates on an oxygen-rich staged combustion closed-cycle system with pump-fed gimbaling. The TH-11 offers a variable thrust range from 50% to 110% and is designed for reusability, capable of at least 30 uses.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.