Statements (157)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Pilot
gptkb:Apollo_program gptkb:space_mission |
| gptkbp:armament |
gptkb:Saturn_V
|
| gptkbp:artwork |
gptkb:Pacific_Ocean
near Hawaii |
| gptkbp:crew |
gptkb:none
|
| gptkbp:duration |
8 hours 36 minutes
8 hours 35 minutes 8 hours, 36 minutes |
| gptkbp:first_flight |
gptkb:Saturn_V_rocket
yes successful uncrewed test flight |
| gptkbp:governed_by |
gptkb:James_E._Webb
|
| gptkbp:has_programs |
gptkb:Apollo_program
|
| https://www.w3.org/2000/01/rdf-schema#label |
Apollo 4
|
| gptkbp:is_tested_for |
yes
positive |
| gptkbp:launch_date |
November 9, 1967
12:00 UTC 7:00 AM EST |
| gptkbp:launch_event |
successful
|
| gptkbp:launch_mass |
approximately 2,900,000 kg
|
| gptkbp:launch_site |
gptkb:Kennedy_Space_Center
|
| gptkbp:launch_vehicle |
gptkb:Saturn_V
gptkb:Saturn_V_rocket heavy-lift rocket |
| gptkbp:launched |
gptkb:Launch_Complex_39_A
|
| gptkbp:manufacturer |
gptkb:North_American_Aviation
gptkb:NASA |
| gptkbp:mission |
gptkb:Johnson_Space_Center
gptkb:none gptkb:Houston gptkb:Apollo_program gptkb:Apollo_5 gptkb:launch_escape_system November 9, 1967 yes data collection completed mission planning successful flight safety operational procedures environmental control systems system redundancy system integration launch operations life support systems stability and control spacecraft systems post-flight analysis communications systems spacecraft recovery performance verification thermal protection systems mission success criteria launch vehicle performance test the launch escape system guidance and control systems performance in space crew safety systems reentry dynamics command module performance engineering evaluation operational validation reentry heat shield service module performance splashdown dynamics demonstrate performance of the spacecraft evaluate the heat shield test the aerodynamic performance test the command module systems test the communication systems test the electrical systems test the environmental control systems test the flight control systems test the ground support systems test the guidance and control systems test the launch operations test the launch vehicle systems test the mission analysis test the mission capabilities test the mission closure test the mission control systems test the mission documentation test the mission evaluation test the mission feedback test the mission follow-up test the mission lessons learned test the mission objectives test the mission operations test the mission performance test the mission planning test the mission reporting test the mission requirements test the mission review test the mission success criteria test the propulsion systems test the recovery operations test the recovery system test the safety systems test the service module systems test the spacecraft systems test the structural integrity test the telemetry systems validate the launch vehicle launch, orbit, reentry |
| gptkbp:mission_duration |
8 hours 36 minutes
8 hours, 35 minutes, 0 seconds 8 hours 35 minutes 8 hours, 36 minutes |
| gptkbp:mission_tested |
reentry and recovery systems
|
| gptkbp:mission_type |
uncrewed
uncrewed test of Apollo spacecraft |
| gptkbp:notable_mission |
demonstrated capabilities for future crewed missions
validated systems for crewed missions first full test of the Apollo spacecraft in flight. |
| gptkbp:objective |
test the Apollo spacecraft
test Saturn V rocket test the Saturn V rocket |
| gptkbp:orbit_type |
gptkb:Earth
2 |
| gptkbp:orbital_altitude |
approximately 300 km
|
| gptkbp:orbital_period |
90 minutes
|
| gptkbp:outcome |
successful
|
| gptkbp:payload_capacity |
gptkb:Apollo_Command_and_Service_Module
gptkb:Command/_Service_Module_(CSM) approximately 30,000 kg approximately 12,000 kg |
| gptkbp:predecessor |
gptkb:Apollo_3
|
| gptkbp:recovery_method |
gptkb:USS_Bennington
|
| gptkbp:related_vehicle |
gptkb:Saturn_V
|
| gptkbp:service |
first uncrewed test of the Apollo spacecraft
first uncrewed flight of Apollo spacecraft |
| gptkbp:significance |
first flight of the Saturn V rocket
first uncrewed test of the Apollo spacecraft |
| gptkbp:spacecraft |
gptkb:Apollo_program
gptkb:Apollo_4 |
| gptkbp:speed |
successful
25,000 miles per hour 6.5 degrees |
| gptkbp:success |
gptkb:true
|
| gptkbp:success_rate |
100%
|
| gptkbp:successor |
gptkb:Apollo_5
|
| gptkbp:was_part_of |
gptkb:spacecraft
gptkb:Apollo_missions |
| gptkbp:bfsParent |
gptkb:Saturn_V
gptkb:KSC_Launch_Complex_34 gptkb:Apollo_Program gptkb:Apollo_program gptkb:The_Apollo_Program gptkb:Saturn_V_rocket gptkb:Neil_Armstrong gptkb:Apollo |
| gptkbp:bfsLayer |
4
|