|
gptkbp:instanceOf
|
rocket stage
|
|
gptkbp:associatedWith
|
moon landing missions
|
|
gptkbp:chemicalFormula
|
liquid oxygen
|
|
gptkbp:controls
|
inertial navigation
|
|
gptkbp:decommissioned
|
1973
|
|
gptkbp:design
|
lightweight structure
|
|
gptkbp:designedBy
|
NASA
|
|
gptkbp:diameter
|
4.0 m
|
|
gptkbp:engine
|
1,000 kN
|
|
gptkbp:engineConfiguration
|
staged combustion
|
|
gptkbp:engineType
|
J-2 engine
|
|
gptkbp:firstFlight
|
gptkb:Apollo_17
gptkb:Apollo_4
|
|
gptkbp:fuelCapacity
|
1,000,000 liters
1,200,000 liters
|
|
gptkbp:fuelType
|
cryogenic
|
|
gptkbp:function
|
upper stage
|
|
gptkbp:gameFeatures
|
liquid hydrogen
|
|
gptkbp:hasDepartment
|
10 minutes
|
|
gptkbp:historicalSignificance
|
enabled human lunar exploration
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
S-IVB
|
|
gptkbp:influenced
|
gptkb:Space_Shuttle_External_Tank
|
|
gptkbp:launched
|
13
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center
45,000 kg
|
|
gptkbp:legacy
|
paved the way for future rockets
|
|
gptkbp:length
|
18.3 m
|
|
gptkbp:manufacturer
|
gptkb:North_American_Aviation
|
|
gptkbp:mission
|
Lunar missions
|
|
gptkbp:notableFeature
|
gptkb:Apollo_16
gptkb:Apollo_15
gptkb:Apollo_17
gptkb:Apollo_8
gptkb:Apollo_11
|
|
gptkbp:numberOfEpisodes
|
5
|
|
gptkbp:operationalArea
|
space exploration
|
|
gptkbp:operationalStatus
|
retired
|
|
gptkbp:payloadCapacity
|
45,000 kg to LEO
|
|
gptkbp:productionCompany
|
1960s
|
|
gptkbp:productionYears
|
1967-1972
|
|
gptkbp:propulsion
|
200,000 lbf
|
|
gptkbp:provides
|
gptkb:Apollo_Guidance_Computer
|
|
gptkbp:reliability
|
not_reusable
|
|
gptkbp:replacedBy
|
S-IVC
|
|
gptkbp:significantEvent
|
first successful test flight
|
|
gptkbp:successor
|
S-IVC
|
|
gptkbp:usedIn
|
gptkb:Apollo_program
gptkb:Saturn_V_rocket
|
|
gptkbp:weight
|
30,000 kg
|