RD872
The RD872 is a single-chamber dual-thrust staged combustion cryogenic rocket engine developed by Yuzhnoye SDO for second stage propulsion applications across the Cyclone-5 and Mayak launch vehicle families. It utilizes tried-and-tested technologies of the Zenit launch vehicle, burning liquid oxygen and kerosene to produce 93 tf of vacuum thrust with a specific impulse of 350.5 […]
Typed specifications6 values
Discloses 5 of 10 fields engineers filter by in this category (category median 3).
- Mass
- 1 530 kg product page
- Thrust
- 912 018 450 mN product page
- Specific impulse
- 350.5 s product page
- Propellant
- oxygen product page kerosene (RP-1)
- TRL
- 6 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 supplier8 lines, in the manufacturer's own wording
- Propellants
- O2 + kerosene
- Vacuum thrust
- 93 tf
- Specific impulse (vacuum)
- 350.5 s
- Propellant mixture ratio
- 2.6
- Number of starts
- 1
- Engine weight (incl. mounts and gimbal actuators)
- 1,530 kg
- Cycle
- Staged combustion, dual-thrust
- TRL
- 6
About
The RD872 is a single-chamber dual-thrust staged combustion cryogenic rocket engine developed by Yuzhnoye SDO for second stage propulsion applications across the Cyclone-5 and Mayak launch vehicle families. It utilizes tried-and-tested technologies of the Zenit launch vehicle, burning liquid oxygen and kerosene to produce 93 tf of vacuum thrust with a specific impulse of 350.5 seconds. The dual-thrust capability allows for throttling to optimize trajectory performance. The RD872 weighs 1,530 kg including mounts and gimbal actuators, and has achieved Technology Readiness Level 6, confirming demonstration in a relevant environment. Its high thrust and specific impulse combination makes it one of the highest-performing LOX/kerosene upper stage engines in Ukraine’s engine portfolio.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.