RD-181

E592136

RD-181 is a Russian-built liquid-fueled rocket engine used to power the first stage of certain orbital launch vehicles, notably Northrop Grumman’s Antares.

All labels observed (1)

Label Occurrences
RD-181 canonical 2

How this entity was disambiguated

Statements (47)

Predicate Object
instanceOf liquid-fueled rocket engine ⓘ
rocket engine ⓘ
application expendable launch vehicles ⓘ
chamberPressure approximately 260 bar ⓘ
combustionChambers 1 ⓘ
control thrust vector control via gimbaling ⓘ
coolingMethod regenerative cooling ⓘ
countryOfOrigin Russia ⓘ
customer Northrop Grumman ⓘ
Orbital ATK ⓘ
derivedFrom RD-191 ⓘ
designedFor medium-lift launch vehicles ⓘ
developer NPO Energomash ⓘ
engineCycle oxidizer-rich staged combustion ⓘ
exportedTo United States ⓘ
fuel RP-1 kerosene ⓘ
gimbalRange up to about 5 degrees ⓘ
ignitionType pyrotechnic ignition system ⓘ
manufacturer NPO Energomash ⓘ
marketedFor commercial launch services ⓘ
nozzleQuantity 1 ⓘ
oxidizer liquid oxygen ⓘ
propellantCombination LOX/RP-1 ⓘ
propellantFeedSystem turbopump-fed ⓘ
propellantType RP-1 kerosene ⓘ
liquid oxygen (LOX) ⓘ
purpose to provide high-performance first-stage propulsion for Antares ⓘ
relatedEngine RD-180 ⓘ
RD-191 ⓘ
replaces AJ26 engines on Antares ⓘ
reusability designed for expendable use ⓘ
role main engine ⓘ
specificImpulseSeaLevel approximately 311 seconds ⓘ
specificImpulseVacuum approximately 339 seconds ⓘ
stage first stage ⓘ
status operational ⓘ
throttleCapability throttleable ⓘ
thrustSeaLevel approximately 1.86 MN ⓘ
thrustVacuum approximately 1.92 MN ⓘ
usedBy United States launch vehicles ⓘ
usedFor orbital launch vehicles first stage propulsion ⓘ
usedFrom mid-2010s ⓘ
usedIn Antares 200-series first stage ⓘ
Antares 230 launch vehicle ⓘ
Antares 230+ launch vehicle ⓘ
usedOn Antares launch vehicle ⓘ
usedOnMission Cygnus cargo resupply missions to the ISS ⓘ

How these facts were elicited

Referenced by (2)

Full triples — surface form annotated when it differs from this entity's canonical label.