DCSS

E930464

DCSS is the cryogenic upper stage used on United Launch Alliance’s Delta IV rockets to perform orbital insertion and mission maneuvers.

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Statements (46)

Predicate Object
instanceOf cryogenic upper stage
rocket stage
abbreviationOf Delta Cryogenic Second Stage NERFINISHED
countryOfOrigin United States of America
surface form: United States
developedFor Delta IV launch system NERFINISHED
engineManufacturer Aerojet Rocketdyne NERFINISHED
engineTypeUsed RL10B-2 NERFINISHED
family Delta Cryogenic Second Stage NERFINISHED
fuelTankType common bulkhead
guidanceSystem inertial guidance
hasConfigurationVariant 4-meter DCSS GENERATED
5-meter DCSS GENERATED
introducedWith Delta IV family NERFINISHED
launchProvider United Launch Alliance NERFINISHED
launchSiteUsedWith Cape Canaveral Space Force Station NERFINISHED
Vandenberg Space Force Base NERFINISHED
manufacturer Boeing
operator United Launch Alliance NERFINISHED
oxidizerType liquid oxygen
primaryFunction orbital insertion
propellantFeedSystem pressure-fed helium pressurization
propellantType liquid hydrogen
propulsionType cryogenic
restartCapability multiple engine restarts
secondaryFunction mission maneuvers
stageCountOnVehicle second stage
status operational
structureMaterial aluminum-lithium alloy
successorOrganizationOperator United Launch Alliance NERFINISHED
typicalMissionRole deployment of satellites GENERATED
inclination change maneuvers GENERATED
payload orbit circularization GENERATED
usedFor geostationary transfer orbit missions
high-energy orbit missions
interplanetary missions
usedOnLaunchVehicle Delta IV NERFINISHED
Delta IV Heavy NERFINISHED
Delta IV Medium NERFINISHED
Delta IV Medium+ (4,2) NERFINISHED
Delta IV Medium+ (5,2) NERFINISHED
usedOnPayloadClass interplanetary probes
military communications satellites
navigation satellites
scientific spacecraft
weather satellites
usesEngineCycle expander cycle

Referenced by (1)

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