RD-120
Sign in to save{(1,125\ \mathrm{kg})(9.807\ \mathrm{m/s^2})}=75.55 Uprated: |length = |diameter = |dry_weight = |used_in = Zenit-2, Zenit-3SL |references = |notes =
Key facts
- Rocket engine.name
- RD-120 (РД-120)
- Rocket engine.country_of_origin
- USSR/Russia
- Rocket engine.manufacturer
- Yuzhmash
- Rocket engine.designer
- NPO Energomash, V.K.Chvanov, V.P. Radovsky
- Rocket engine.status
- Operational
- Rocket engine.purpose
- Upper stage
- Rocket engine.type
- liquid
- Rocket engine.fuel
- RP-1
- Rocket engine.oxidiser
- LOX
- Rocket engine.cycle
- Staged combustion cycle
- Rocket engine.thrust(Vac)
- Standard: Uprated:
- Rocket engine.burn_time
- 315 seconds
- Rocket engine.chamber_pressure
- Standard: Uprated:
- Rocket engine.thrust_to_weight
- Standard: \frac{833,565\ \mathrm{N
via Wikipedia infobox
Article
12 sectionsContents
- History
- Versions
- Technological derivatives
- RD-170 family
- RD-801 and RD-810
- SCE-200
- YF-100 and YF-115
- Derivatives comparison
- See also
- References
- Notes
- External links
The RD-120 (, GRAU index: 11D123) is a liquid upper stage rocket engine burning RG-1 (refined kerosene) and LOX in an oxidizer rich staged combustion cycle with an O/F ratio of 2.6. It is used in the second stage of the Zenit family of launch vehicles. It has a single, fixed combustion chamber and thus on the Zenit it is paired with the RD-8 vernier engine. The engine was developed from 1976 to 1985 by NPO Energomash with V.P. Radovsky leading the development. It is manufactured by, among others, Yuzhmash in Ukraine.
It should not be confused with the RD-0120, which is a discontinued LOX/hydrogen rocket engine that was used in the Soviet Energia launch system.