Statements (48)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Command_Line_Interface
|
| gptkbp:ascent_module |
no
|
| gptkbp:communication |
S-band radio
|
| gptkbp:crew |
gptkb:James_Lovell
gptkb:Frank_Borman gptkb:William_Anders |
| gptkbp:crew_capacity |
gptkb:3
|
| gptkbp:diameter |
12.8 feet
|
| gptkbp:first_manned_mission_to |
gptkb:the_Moon
|
| gptkbp:homeworld |
December 27, 1968
|
| https://www.w3.org/2000/01/rdf-schema#label |
Apollo 8 Command Module
|
| gptkbp:landing_site |
gptkb:Pacific_Ocean
|
| gptkbp:launch_site |
gptkb:Kennedy_Space_Center
|
| gptkbp:launch_vehicle |
gptkb:Saturn_V
|
| gptkbp:launched |
December 21, 1968
|
| gptkbp:length |
11.3 feet
|
| gptkbp:manufacturer |
gptkb:North_American_Aviation
|
| gptkbp:mission |
test lunar orbit
achieve a successful reentry from lunar orbit be a precursor to Apollo 11 be a significant milestone in space exploration. broadcast live television from lunar orbit carry a Christmas message carry a crew of three astronauts complete a lunar flyby conduct a mission without a lunar lander demonstrate the feasibility of lunar missions execute a lunar orbit insertion maneuver inspire future lunar exploration missions perform a translunar injection return safely to Earth after lunar orbit test the Apollo Lunar Module's systems test the Apollo spacecraft's systems in deep space |
| gptkbp:mission_duration |
6 days
|
| gptkbp:mission_type |
crewed lunar orbit
|
| gptkbp:module |
no
|
| gptkbp:orbital_altitude |
60 miles
|
| gptkbp:part_of |
Apollo 8 mission
|
| gptkbp:power_source |
fuel cells
|
| gptkbp:predecessor |
gptkb:Apollo_7_Command_Module
|
| gptkbp:recovery_method |
gptkb:USS_Yorktown
|
| gptkbp:service |
orbit the Moon
|
| gptkbp:speed |
25,000 mph
|
| gptkbp:successor |
gptkb:Apollo_9_Command_Module
|
| gptkbp:used_for |
manned spaceflight
|
| gptkbp:weight |
5,000 pounds
|
| gptkbp:bfsParent |
gptkb:Apollo_9_Command_Module
|
| gptkbp:bfsLayer |
7
|