|
gptkbp:instanceOf
|
gptkb:satellite
|
|
gptkbp:commandModuleCrewStations
|
3
|
|
gptkbp:commandModuleDockingSystem
|
probe and drogue
|
|
gptkbp:commandModuleGuidance
|
gptkb:Apollo_Guidance_Computer
|
|
gptkbp:commandModuleHatch
|
side and docking hatches
|
|
gptkbp:commandModuleHeatShield
|
ablative
|
|
gptkbp:commandModuleParachutes
|
3 main, 2 drogue
|
|
gptkbp:commandModuleRecovery
|
splashdown
|
|
gptkbp:commandModuleVolume
|
6.17 m³
|
|
gptkbp:commandModuleWindows
|
5
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:diameter
|
3.9 m
|
|
gptkbp:firstFlight
|
gptkb:Apollo_7
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Apollo Block II CSM
|
|
gptkbp:lastFlight
|
gptkb:Apollo–Soyuz_Test_Project
|
|
gptkbp:launchVehicle
|
gptkb:Saturn_IB
gptkb:Saturn_V
|
|
gptkbp:length
|
11.0 m
|
|
gptkbp:manufacturer
|
gptkb:North_American_Aviation
|
|
gptkbp:mass
|
~30,300 kg
|
|
gptkbp:material
|
aluminum alloy
aluminum honeycomb structure
|
|
gptkbp:missionsFlown
|
12
|
|
gptkbp:notableMission
|
gptkb:Apollo_11
gptkb:Apollo_12
gptkb:Skylab_2
gptkb:Skylab_3
gptkb:Skylab_4
gptkb:Apollo_10
gptkb:Apollo_16
gptkb:Apollo_13
gptkb:Apollo_17
gptkb:Apollo_7
gptkb:Apollo_8
gptkb:Apollo–Soyuz_Test_Project
gptkb:Apollo_14
gptkb:Apollo_15
gptkb:Apollo_9
|
|
gptkbp:numberBuilt
|
17
|
|
gptkbp:predecessor
|
gptkb:Apollo_Block_I_CSM
|
|
gptkbp:seatingCapacity
|
3
|
|
gptkbp:serviceModuleFuelCells
|
3 hydrogen-oxygen fuel cells
|
|
gptkbp:serviceModuleMainEngine
|
gptkb:AJ10-137
|
|
gptkbp:serviceModulePropulsion
|
gptkb:Service_Propulsion_System_(SPS)
|
|
gptkbp:serviceModuleRCS
|
reaction control system
|
|
gptkbp:serviceModuleVolume
|
6.0 m³
|
|
gptkbp:shape
|
blunt cone
|
|
gptkbp:successor
|
none
|
|
gptkbp:usedIn
|
gptkb:Apollo_program
gptkb:Skylab_program
gptkb:Apollo–Soyuz_Test_Project
|
|
gptkbp:bfsParent
|
gptkb:Apollo_Command/Service_Module_CSM-101
|
|
gptkbp:bfsLayer
|
6
|