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.

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All labels observed (1)

Label Occurrences
Service Propulsion System canonical 1

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 of America
surface form: United States
designedFor deep-space operations
high-reliability crewed missions
developedBy Aerojet Rocketdyne
surface form: Aerojet
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 Johnson Space Center
surface form: NASA Manned Spacecraft Center
oxidizer nitrogen tetroxide
partOf Apollo command and service module
surface form: 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
surface form: Apollo Command and Service Module

Referenced by (1)

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

Apollo 12 serviceModuleEngine Service Propulsion System