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 program ⓘ
linked to: Ariane 5
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 configuration ⓘ
linked to: Ariane 5 ECA
launchVehicleFamily Ariane 5 ⓘ
manufacturer Airbus Defence and Space ⓘ
linked to: Astrium

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.