gptkbp:instance_of
|
gptkb:Lunar_Module
|
gptkbp:aircraft_operated
|
8 days, 3 hours, 42 minutes
|
gptkbp:communication_system
|
S-band radio
|
gptkbp:control_surfaces
|
reaction control thrusters
|
gptkbp:control_system
|
gptkb:navigation_system
|
gptkbp:crew
|
gptkb:none
|
gptkbp:crew_capacity
|
gptkb:none
|
gptkbp:designed_by
|
gptkb:Grumman_Aircraft_Engineering_Corporation
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
gptkbp:first_ascent
|
yes
3,500 pounds
|
gptkbp:first_flight
|
gptkb:LM-2
gptkb:Apollo_5
successful
uncrewed
January 31, 1966
demonstrated lunar landing capabilities
demonstrate lunar landing capabilities
first flight of a lunar module
lunar landing simulation
|
gptkbp:fuel_type
|
hypergolic propellants
|
gptkbp:height
|
7.5 meters
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lunar Module 2
|
gptkbp:is_tested_for
|
gptkb:Saturn_IB
|
gptkbp:landing_distance
|
four
|
gptkbp:landing_legs_type
|
retractable
|
gptkbp:landing_site
|
gptkb:Earth
|
gptkbp:launch_site
|
gptkb:Cape_Kennedy_Air_Force_Station
|
gptkbp:launch_vehicle
|
gptkb:Saturn_IB
|
gptkbp:launched
|
January 31, 1966
|
gptkbp:manufacturer
|
gptkb:Grumman
|
gptkbp:mission
|
gptkb:Apollo_5
successful
|
gptkbp:mission_duration
|
8 days
|
gptkbp:mission_type
|
uncrewed test flight
|
gptkbp:module
|
yes
|
gptkbp:operational_status
|
retired
|
gptkbp:orbital_altitude
|
100 kilometers
|
gptkbp:part_of
|
gptkb:Apollo_program
|
gptkbp:power_source
|
fuel cells
|
gptkbp:propulsion
|
10,000 pounds
|
gptkbp:successor
|
gptkb:Lunar_Module_3
|
gptkbp:test_flight_communications_system
|
S-band radio
|
gptkbp:test_flight_control_system
|
gptkb:navigation_system
|
gptkbp:test_flight_engine_type
|
gptkb:Team_Rocket
|
gptkbp:test_flight_height
|
7.5 meters
|
gptkbp:test_flight_mission_type
|
uncrewed
|
gptkbp:test_flight_power_source
|
fuel cells
|
gptkbp:test_flight_weight
|
15,000 pounds
|
gptkbp:weight
|
15,000 pounds
|
gptkbp:weight_at_launch
|
15,000 pounds
|
gptkbp:bfsParent
|
gptkb:Eagle_lunar_module
|
gptkbp:bfsLayer
|
5
|