gptkbp:instance_of
|
gptkb:spacecraft
gptkb:Lunar_Module
|
gptkbp:ascent_stage_weight
|
10,000 pounds
|
gptkbp:commander
|
gptkb:Neil_Armstrong
|
gptkbp:communication_system
|
gptkb:radio_station
S-band radio
|
gptkbp:control_system
|
gptkb:navigation_system
manual and automatic
|
gptkbp:court
|
two-stage
Two-stage spacecraft
|
gptkbp:crew
|
gptkb:Harrison_Schmitt
gptkb:David_Scott
gptkb:Buzz_Aldrin
gptkb:Alan_Shepard
gptkb:Charles_Duke
gptkb:John_Young
gptkb:Eugene_Cernan
gptkb:Neil_Armstrong
gptkb:Ken_Mattingly
gptkb:Alan_Bean
gptkb:Jack_Swigert
gptkb:Fred_Haise
|
gptkbp:crew_capacity
|
2
2 astronauts
|
gptkbp:cultural_impact
|
inspired films and literature
symbol of space exploration
icon of the Apollo program
|
gptkbp:descent_stage_weight
|
5,750 pounds
|
gptkbp:design_purpose
|
to land on and take off from the Moon
|
gptkbp:designed_by
|
gptkb:Grumman_Aircraft_Engineering_Corporation
gptkb:NASA
|
gptkbp:diameter
|
4.2 meters
|
gptkbp:elevation
|
approximately 100 kilometers
|
gptkbp:emergency_services
|
gptkb:Buzz_Aldrin
gptkb:Apollo_17
gptkb:Neil_Armstrong
gptkb:Apollo_11
July 20, 1969
December 11, 1972
|
gptkbp:first_ascent
|
gptkb:Lunar_Module_Ascent_Engine
8 minutes
Used for returning to orbit
3,500 pounds
used for returning to orbit
|
gptkbp:first_flight
|
gptkb:Buzz_Aldrin
gptkb:Apollo_17
gptkb:Apollo_9
gptkb:Neil_Armstrong
gptkb:Apollo_5
|
gptkbp:flight_style
|
gptkb:17
|
gptkbp:has_units
|
gptkb:15
|
gptkbp:height
|
7.2 m
23 feet
7.1 meters
|
gptkbp:homeworld
|
via Command Module
|
https://www.w3.org/2000/01/rdf-schema#label
|
Apollo Lunar Module
|
gptkbp:influenced_by
|
Lunar exploration technology
|
gptkbp:inspiration
|
gptkb:Mars_landers
Spacecraft design
Future lunar missions
future lunar landers
|
gptkbp:landing_capability
|
lunar surface
|
gptkbp:landing_distance
|
gptkb:4
four
6 successful landings
1.6 m/s
15,750 pounds
|
gptkbp:landing_site
|
gptkb:12
gptkb:Apollo_11
gptkb:Sea_of_Tranquility
|
gptkbp:last_lunar_landing
|
gptkb:Apollo_17
|
gptkbp:last_successful_landing
|
December 11, 1972
|
gptkbp:launch_mass
|
15,200 kg
|
gptkbp:launch_vehicle
|
gptkb:Saturn_V
|
gptkbp:legacy
|
paved the way for future lunar exploration
pioneered lunar exploration technology
first crewed lunar landing vehicle
|
gptkbp:manufacturer
|
gptkb:Grumman_Aircraft_Engineering_Corporation
|
gptkbp:mission
|
gptkb:Apollo_14
gptkb:Apollo_16
gptkb:6
gptkb:Houston,_Texas
gptkb:Apollo_15
gptkb:Apollo_17
gptkb:Apollo_11
gptkb:Apollo_12
December 14, 1972
12 astronauts
|
gptkbp:mission_duration
|
8 days, 3 hours, 18 minutes
|
gptkbp:module
|
gptkb:Eagle
gptkb:Challenger
gptkb:Falcon
gptkb:Buzz_Aldrin
gptkb:Orion
gptkb:Lunar_Module
gptkb:Antares
gptkb:Intrepid
yes
12 minutes
used for landing on the Moon
Approximately 75 hours
Used for landing on the Moon
up to 3 days
up to 75 hours
Lunar Module Commander
|
gptkbp:name
|
gptkb:Challenger
|
gptkbp:notable_achievement
|
first human landing on the Moon
|
gptkbp:operational_period
|
1969-1972
approximately 2.5 hours
|
gptkbp:operational_status
|
retired
|
gptkbp:power_source
|
Fuel cells
fuel cells
|
gptkbp:primary_function
|
Lunar landing and ascent
|
gptkbp:primary_mission
|
gptkb:Mars_Rover
Lunar landing
Lunar ascent
lunar ascent
|
gptkbp:propulsion
|
gptkb:Lunar_Module_Descent_Engine
gptkb:Team_Rocket
10,000 pounds
Hypergolic propellants
hypergolic propellants
|
gptkbp:related_to
|
gptkb:Mars_Rover
gptkb:Apollo_program
gptkb:vehicles
gptkb:NASA_missions
gptkb:Lunar_exploration
gptkb:Space_race
Human spaceflight
Lunar exploration missions
Lunar surface operations
Lunar ascent stage
Lunar descent stage
Lunar module docking
Robotic lunar landers
|
gptkbp:related_vehicle
|
no
|
gptkbp:research
|
conducted on the Moon
|
gptkbp:retired
|
gptkb:1972
|
gptkbp:scientific_instruments
|
gptkb:magnetometer
TV camera
lunar soil scoop
laser ranging retroreflector
soil mechanics tester
moon rock sample return system
|
gptkbp:significance
|
first crewed vehicle to land on another celestial body
|
gptkbp:significant_event
|
gptkb:First_human_landing_on_the_Moon
Last human landing on the Moon
|
gptkbp:successor
|
gptkb:none
gptkb:Orion_Multi-Purpose_Crew_Vehicle
|
gptkbp:used_in
|
gptkb:Apollo_14
gptkb:Apollo_16
gptkb:Apollo_program
gptkb:Apollo_15
gptkb:Apollo_17
gptkb:Apollo_12
|
gptkbp:weight
|
15,200 pounds
15,750 kg
|
gptkbp:weight_on_earth
|
approximately 15,750 pounds
|
gptkbp:weight_on_launch
|
29,000 pounds
|
gptkbp:weight_on_moon
|
approximately 2,400 pounds
|
gptkbp:width
|
4.2 m
14 feet
4.2 meters
|
gptkbp:bfsParent
|
gptkb:NASA
|
gptkbp:bfsLayer
|
3
|