|
gptkbp:instanceOf
|
rocket
|
|
gptkbp:crewCapacity
|
3
|
|
gptkbp:designedBy
|
NASA
|
|
gptkbp:engineType
|
F-1
J-2
|
|
gptkbp:firstAwarded
|
S-IC
|
|
gptkbp:firstClaim
|
gptkb:S-IVB
|
|
gptkbp:firstFlight
|
1967-11-09
1975-07-15
|
|
gptkbp:firstMatch
|
S-II
|
|
gptkbp:fuelType
|
RP-1_and_Liquid_Oxygen
|
|
gptkbp:height
|
363 feet
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Saturn V rocket
|
|
gptkbp:influencedBy
|
gptkb:Titan_rocket
gptkb:Atlas_rocket
Redstone rocket
R-7 Semyorka
V-2 rocket
|
|
gptkbp:inspiration
|
gptkb:Space_Launch_System
|
|
gptkbp:launched
|
$1 billion
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center
2,800,000 kg
|
|
gptkbp:launchVehicle
|
heavy-lift launch vehicle
|
|
gptkbp:majorRivers
|
13
|
|
gptkbp:manufacturer
|
gptkb:IBM
gptkb:Boeing
gptkb:North_American_Aviation
Rocketdyne
|
|
gptkbp:notableFeature
|
gptkb:Skylab
gptkb:Apollo_17
gptkb:Apollo_11
|
|
gptkbp:number_of_stages
|
3
|
|
gptkbp:payloadCapacity
|
140,000 kg to Low Earth Orbit
|
|
gptkbp:productionYears
|
1967-1975
|
|
gptkbp:retired
|
1975
|
|
gptkbp:succeededBy
|
100%
|
|
gptkbp:usedFor
|
gptkb:Apollo_program
|
|
gptkbp:usedIn
|
gptkb:Apollo_14
gptkb:Apollo_10
gptkb:Apollo_16
gptkb:Apollo_6
gptkb:Apollo_2
gptkb:Apollo_3
gptkb:Skylab_3
gptkb:Skylab_4
gptkb:Apollo_15
gptkb:Apollo_8
gptkb:Apollo_7
gptkb:Apollo_9
gptkb:Apollo_13
gptkb:Apollo_5
gptkb:Skylab_2
gptkb:Apollo-Soyuz_Test_Project
gptkb:Apollo_lunar_missions
gptkb:Apollo_4
gptkb:Apollo_1
Skylab_missions
Apollo_17_lunar_landing
Apollo_11_lunar_landing
|
|
gptkbp:weight
|
2,800,000 pounds
|