ESC-A

E290059

ESC-A is the cryogenic upper stage used on the Ariane 5 ECA launch vehicle, powered by a single HM7B engine to place payloads into orbit.

All labels observed (1)

Label Occurrences
ESC-A canonical 1

How this entity was disambiguated

Statements (47)

Predicate Object
instanceOf Ariane 5 upper stage
cryogenic upper stage
rocket stage
controlSystem hydrazine reaction control system
countryOfOrigin France
developedFor Ariane 5
surface form: Ariane 5 program
engineConfiguration single HM7B engine
engineCount 1
engineManufacturer Safran Aircraft Engines
engineThrustClass tens of kilonewtons
fuel liquid hydrogen
guidanceType inertial guidance
introducedOnVehicleVariant Ariane 5 ECA
launchPad ELA-3
launchServiceProvider Arianespace
launchSite Guiana Space Centre
launchVehicleConfiguration Ariane 5 ECA
surface form: Ariane 5 ECA configuration
launchVehicleFamily Ariane 5
manufacturer Astrium
surface form: Airbus Defence and Space

ArianeGroup
missionPhase orbit circularization
post-core-stage ascent
operator Arianespace
orbitTypesSupported GTO
HEO
LEO
oxidizer liquid oxygen
partOf Ariane 5 ECA
poweredBy HM7B
primaryFunction geostationary transfer orbit insertion
insertion of payloads into orbit
propellantCombination liquid oxygen–liquid hydrogen
propellantState liquid
propellantType cryogenic
propulsionCycle expander cycle
replaces EPS upper stage on some Ariane 5 variants
role upper stage
stageNumber 3
status operational
successor ESC-B
typicalPayloads communications satellites
scientific spacecraft
usedFor commercial satellite launches
government payload launches
usedOnLaunchVehicle Ariane 5 ECA
usedWithBoosters EAP solid rocket boosters
usedWithCoreStage EPC cryogenic core stage

How these facts were elicited

Referenced by (1)

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