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gptkbp:instance_of
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gptkb:software
|
|
gptkbp:bfsLayer
|
3
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gptkbp:bfsParent
|
gptkb:Apollo_7
|
|
gptkbp:artwork
|
gptkb:Pacific_Ocean
November 24, 1966
|
|
gptkbp:command_structure
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gptkb:software
|
|
gptkbp:crew
|
gptkb:3
gptkb:Frank_Borman
gptkb:James_A._Lovell_Jr.
gptkb:William_Anders
demonstrated crew safety protocols
extensive training prior to flight
valuable crew experience gained
|
|
gptkbp:debut_year
|
first launch of Apollo Command/ Service Module
|
|
gptkbp:duration
|
14 days, 1 hour, 49 minutes
|
|
gptkbp:elevation
|
Low Earth Orbit
|
|
gptkbp:events
|
successful launch
|
|
gptkbp:first_flight
|
gptkb:software
gptkb:Apollo_1
data collected for future missions
collected flight data
first crewed test flight of Apollo program
planned flight path
|
|
gptkbp:has_programs
|
gptkb:software
|
|
gptkbp:historical_significance
|
historically significant mission
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Apollo CSM-101
|
|
gptkbp:is_tested_for
|
conducted engineering tests during flight
|
|
gptkbp:landing_site
|
gptkb:Pacific_Ocean
|
|
gptkbp:launch_date
|
12:00 PMEST
November 9, 1966
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Saturn_IB
|
|
gptkbp:launched
|
gptkb:Launch_Complex_37_B
November 9, 1966
|
|
gptkbp:manufacturer
|
gptkb:North_American_Aviation
|
|
gptkbp:mission
|
gptkb:spacecraft
gptkb:Houston,_Texas
successful
crewed test flight
paved the way for lunar missions
Low Earth Orbit mission
post-mission report generated
test systems and procedures for future missions
|
|
gptkbp:mission_duration
|
14 days
|
|
gptkbp:part_of
|
gptkb:software
|
|
gptkbp:propulsion
|
gptkb:Command/_Service_Module
tested spacecraft design
|
|
gptkbp:restoration
|
gptkb:USS_Essex
successful recovery operation
|
|
gptkbp:services
|
gptkb:Apollo_Service_Module
|
|
gptkbp:significance
|
demonstrated capabilities for future lunar missions
|
|
gptkbp:significant_event
|
first crewed flight of Apollo spacecraft
|
|
gptkbp:speed
|
November 24, 1966
|
|
gptkbp:successor
|
gptkb:Apollo_CSM-102
|