|
gptkbp:instance_of
|
gptkb:Lunar_Module
|
|
gptkbp:ascent_stage_mass
|
2,000 kg
|
|
gptkbp:communication_system
|
S-band radio
|
|
gptkbp:control_system
|
Fly-by-wire
|
|
gptkbp:crew
|
gptkb:David_Scott
gptkb:James_Irwin
|
|
gptkbp:descent_stage_mass
|
4,500 kg
|
|
gptkbp:designed_by
|
gptkb:Grumman_Aircraft_Engineering_Corporation
|
|
gptkbp:emergency_services
|
gptkb:Apollo_17
gptkb:Apollo_11
|
|
gptkbp:first_flight
|
gptkb:Apollo_17
gptkb:Apollo_9
|
|
gptkbp:height
|
7.2 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lunar Module 91
|
|
gptkbp:landing_distance
|
Soft landing
|
|
gptkbp:landing_site
|
gptkb:6
gptkb:Hadley-Apennine
July 30, 1971
|
|
gptkbp:launch_date
|
July 26, 1971
|
|
gptkbp:launch_vehicle
|
gptkb:Saturn_V
|
|
gptkbp:manufacturer
|
gptkb:Northrop_Grumman
|
|
gptkbp:mission
|
gptkb:17
gptkb:Apollo_15
|
|
gptkbp:mission_duration
|
75 hours
|
|
gptkbp:mission_type
|
gptkb:Manned_lunar_landing
|
|
gptkbp:module
|
gptkb:3
|
|
gptkbp:navigation_system
|
Inertial navigation system
|
|
gptkbp:operational_status
|
Retired
|
|
gptkbp:part_of
|
gptkb:Apollo_program
|
|
gptkbp:power_source
|
Fuel cells
|
|
gptkbp:propulsion
|
Hypergolic propellants
|
|
gptkbp:research
|
gptkb:Lunar_Roving_Vehicle
|
|
gptkbp:sampled_in
|
77 kg of lunar material
|
|
gptkbp:total_lunar_evahours
|
18.5
|
|
gptkbp:width
|
4.2 m
|
|
gptkbp:bfsParent
|
gptkb:Apollo_91_spacecraft
|
|
gptkbp:bfsLayer
|
7
|