Service Propulsion System

E256003

The Service Propulsion System was the main rocket engine of the Apollo Service Module, used for major course corrections, lunar orbit insertion, and trans-Earth injection during Apollo missions.

All labels observed (1)

Label Occurrences
Service Propulsion System canonical 3

How this entity was disambiguated

Statements (48)

Predicate Object
instanceOf rocket engine ⓘ
spacecraft propulsion system ⓘ
combustionCycle pressure-fed ⓘ
controlledBy Apollo Guidance Computer ⓘ
Service Module reaction control system valves ⓘ
countryOfOrigin United States ⓘ
designedFor deep-space operations ⓘ
high-reliability crewed missions ⓘ
developedBy Aerojet ⓘ
linked to: Aerojet Rocketdyne
fuel Aerozine 50 ⓘ
heritage Aerojet AJ10 engine family ⓘ
locatedIn Service Module engine bay ⓘ
missionPhase abort-to-Earth maneuvers ⓘ
lunar orbit departure burns ⓘ
lunar orbit insertion burns ⓘ
midcourse corrections ⓘ
translunar injection corrections ⓘ
mountingLocation rear of Apollo Service Module ⓘ
nozzleType fixed nozzle ⓘ
operatedBy NASA ⓘ
operator NASA Manned Spacecraft Center ⓘ
oxidizer nitrogen tetroxide ⓘ
partOf Apollo Service Module ⓘ
primaryFunction service module main propulsion ⓘ
propellantType hypergolic ⓘ
restartCapability multiple restarts ⓘ
safetyFeature hypergolic ignition reliability ⓘ
pressure-fed simplicity ⓘ
status retired ⓘ
throttleCapability non-throttleable ⓘ
usedFor lunar orbit insertion ⓘ
major course corrections ⓘ
trans-Earth injection ⓘ
usedInProgram Apollo program ⓘ
usedOnMission Apollo 10 ⓘ
Apollo 11 ⓘ
Apollo 12 ⓘ
Apollo 13 ⓘ
Apollo 14 ⓘ
Apollo 15 ⓘ
Apollo 16 ⓘ
Apollo 17 ⓘ
Apollo 7 ⓘ
Apollo 8 ⓘ
Apollo 9 ⓘ
Apollo–Soyuz Test Project ⓘ
usedOnMissionType crewed lunar missions ⓘ
usedOnVehicle Apollo Command and Service Module ⓘ

How these facts were elicited

Referenced by (3)

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

Apollo 12 → serviceModuleEngine → Service Propulsion System ⓘ
CSM-110 → primaryEngine → Service Propulsion System ⓘ
Block I Command and Service Module → primaryPropulsion → Service Propulsion System ⓘ