|
gptkbp:instance_of
|
gptkb:Author
|
|
gptkbp:allows
|
Limited to lunar missions
|
|
gptkbp:challenges
|
Weight and stability
|
|
gptkbp:communication
|
Radio system
|
|
gptkbp:controls
|
Guidance and Navigation System
Manual and automated controls
|
|
gptkbp:cooling_system
|
Insulation
|
|
gptkbp:crew
|
2
Sample collection
Extensive training required
Astronauts trained for lunar conditions
|
|
gptkbp:design
|
gptkb:Grumman_Aircraft_Engineering_Corporation
Ascent from lunar surface
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:elevation
|
Throttleable engine
|
|
gptkbp:engine_type
|
gptkb:F-1_engine
|
|
gptkbp:first_flight
|
gptkb:Apollo_17
gptkb:Apollo_11
|
|
gptkbp:fuel_capacity
|
2,000 pounds
|
|
gptkbp:fuel_type
|
Hypergolic propellants
|
|
gptkbp:game_world
|
gptkb:battle
|
|
gptkbp:height
|
4.2 meters
|
|
gptkbp:historical_significance
|
gptkb:First_manned_lunar_ascent_vehicle
|
|
gptkbp:home_port
|
gptkb:Author
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lunar Module ascent stage
|
|
gptkbp:instrument
|
gptkb:Limited
|
|
gptkbp:is_a_destination_for
|
gptkb:physicist
|
|
gptkbp:is_used_for
|
gptkb:planet
|
|
gptkbp:landing_gear
|
Retractable landing gear
|
|
gptkbp:landing_site
|
Lunar surface
|
|
gptkbp:launch_date
|
1969-1972
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Saturn_V
15,000 pounds
|
|
gptkbp:launched
|
Pre-launch checks required
|
|
gptkbp:max_takeoff_weight
|
Sample return to Command Module
|
|
gptkbp:mission
|
gptkb:Houston,_Texas
Remains on lunar surface
|
|
gptkbp:mission_duration
|
varied by mission
Apollo 11, 12, 14, 15, 16, 17
|
|
gptkbp:navigation_system
|
Inertial navigation system
|
|
gptkbp:number_of_stages
|
gptkb:battle
|
|
gptkbp:operated_by
|
gptkb:spacecraft
|
|
gptkbp:operating_hours
|
approximately 8 hours
|
|
gptkbp:operational_area
|
Lunar atmosphere
|
|
gptkbp:operational_history
|
1969-1972
|
|
gptkbp:part_of
|
gptkb:software
|
|
gptkbp:power_output
|
Batteries
|
|
gptkbp:propulsion
|
gptkb:rocket
|
|
gptkbp:safety_features
|
Abort system
|
|
gptkbp:scholarships
|
gptkb:battle
|
|
gptkbp:speed
|
Not applicable
|
|
gptkbp:status
|
Decommissioned
|
|
gptkbp:succeeded_by
|
100% in Apollo missions
|
|
gptkbp:surface
|
RCS thrusters
|
|
gptkbp:weight
|
4,500 kg
Balanced for ascent
|
|
gptkbp:width
|
4.2 meters
|
|
gptkbp:bfsParent
|
gptkb:Apollo_11_artifacts
|
|
gptkbp:bfsLayer
|
4
|