|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:average_temperature
|
-40 to 120 degrees Fahrenheit
|
|
gptkbp:components
|
gptkb:Lunar_Module_Ascent_Stage
gptkb:Lunar_Module
|
|
gptkbp:constructed_in
|
1960s
|
|
gptkbp:control_system
|
gptkb:Lunar_Module_Guidance_Computer
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:designed_for
|
low-gravity environment
|
|
gptkbp:first_introduced
|
gptkb:Apollo_11
|
|
gptkbp:fuel_type
|
hypergolic propellant
|
|
gptkbp:function
|
attitude control
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lunar Module RCS Thrusters
|
|
gptkbp:ignition_system
|
spontaneous
|
|
gptkbp:influenced_by
|
jet propulsion
early rocket technology
|
|
gptkbp:investment
|
300 psi
|
|
gptkbp:is_accessible_by
|
gptkb:Lunar_Module
|
|
gptkbp:is_critical_for
|
gptkb:navigation
safe landing
safe ascent
|
|
gptkbp:is_integrated_with
|
Lunar Module systems
|
|
gptkbp:mission
|
gptkb:Mars_Rover
lunar orbit
lunar ascent
|
|
gptkbp:number_of_thrusters
|
gptkb:16
|
|
gptkbp:operated_by
|
gptkb:astronaut
|
|
gptkbp:operational_status
|
manual and automatic
|
|
gptkbp:propulsion
|
100 pounds
|
|
gptkbp:provides
|
pitch, yaw, and roll control
|
|
gptkbp:related_to
|
gptkb:space_exploration
gptkb:Moon
gptkb:Apollo_lunar_missions
gptkb:lunar_landers
propulsion systems
aerospace engineering
spacecraft design
spacecraft attitude control
rocket science
spacecraft systems
spacecraft propulsion
thrust vector control
spacecraft maneuvering
NASA technology
|
|
gptkbp:replaced_by
|
modern spacecraft thrusters
|
|
gptkbp:safety_features
|
redundancy
|
|
gptkbp:tested_at
|
gptkb:NASA_Marshall_Space_Flight_Center
|
|
gptkbp:type
|
monomethylhydrazine and nitrogen tetroxide
|
|
gptkbp:used_for
|
maneuvering in space
|
|
gptkbp:used_in
|
gptkb:Apollo_program
gptkb:Apollo_17
|
|
gptkbp:weight
|
approximately 1.5 pounds each
|
|
gptkbp:bfsParent
|
gptkb:Apollo_Lunar_Module_Guidance_Computer
|
|
gptkbp:bfsLayer
|
7
|