TH-12V
Space Pioneer (Tianbing Technology)
The TH-12V is a hundred-ton class liquid oxygen/kerosene engine designed for reusable medium and large liquid launch vehicles.
Typed specifications3 values
Discloses 2 of 10 fields engineers filter by in this category (category median 3).
- Specific impulse
- 346 s product page
- Propellant
- oxygen product page kerosene (RP-1)
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 supplier8 lines, in the manufacturer's own wording
- Propellant
- Liquid Oxygen + Kerosene
- Sea-level thrust
- 110 t
- Vacuum specific impulse
- 346 s
- Thrust-to-weight ratio
- 115
- Number of ignitions
- 2 times
- System
- Gas generator cycle
- Gimbaling method
- Pump-fed gimbal
- Number of reuses
- ≥10
About
The TH-12V is part of the Tianhuo series of liquid rocket engines developed by Space Pioneer (Tianbing Technology). This hundred-ton class engine utilizes liquid oxygen and kerosene as propellants, making it suitable for reusable medium and large liquid launch vehicles. It features a gas generator cycle system and a pump-fed gimbaling mechanism. The engine boasts a sea-level thrust of 110 tons and a vacuum specific impulse of 346 seconds, with a thrust-to-weight ratio of 115. It is designed for multiple ignitions, with a capability of at least 10 reuses.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.