Lunar Module 2

GPTKB entity

Statements (53)
Predicate Object
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