Apollo Service Module

GPTKB entity

Statements (61)
Predicate Object
gptkbp:instance_of gptkb:spacecraft
gptkbp:contains gptkb:Environmental_Protection_Agency
gptkb:Service_Propulsion_System
gptkb:communication_systems
Electrical Power System
gptkbp:control_system gptkb:Inertial_Navigation_System
gptkbp:cooling_system Radiator system
gptkbp:crew_capacity 3 astronauts
gptkbp:designed_by gptkb:North_American_Aviation
gptkbp:diameter 4.2 m
gptkbp:first_introduced gptkb:Apollo_7
gptkbp:fuel_type Hypergolic propellant
https://www.w3.org/2000/01/rdf-schema#label Apollo Service Module
gptkbp:is_capable_of supporting a crew of three
gptkbp:is_designed_for deep space missions
gptkbp:is_designed_to ensure mission success
enable lunar exploration
return safely to Earth
withstand re-entry heat
be jettisoned before re-entry
facilitate crew safety
support scientific experiments
gptkbp:is_equipped_with Solar panels
Battery systems
Navigation aids
Guidance system
Waste management system
Thermal control systems
Structural framework
Oxygen system
Telemetry system
Emergency systems
Communication antennas
Water recovery system
RCS thrusters
gptkbp:is_part_of gptkb:Apollo_Lunar_Module
gptkb:Apollo_program
gptkbp:is_used_for lunar missions
gptkbp:is_used_to transport astronauts
provide life support during missions
provide power to the Command Module
provide propulsion for the mission
support lunar landings
gptkbp:launched gptkb:Saturn_V_rocket
gptkbp:launched_in gptkb:Kennedy_Space_Center
gptkbp:length 6.9 m
gptkbp:manufacturer gptkb:Rockwell_International
gptkbp:mass 4,500 kg
gptkbp:operational_period 1967-1972
gptkbp:part_of gptkb:Apollo_program
gptkbp:provides gptkb:power
propulsion
communications
life support
gptkbp:retired gptkb:1972
gptkbp:storage Consumables storage
gptkbp:succeeded_by gptkb:Orion_spacecraft
gptkbp:used_in gptkb:Apollo_17
gptkb:Apollo_missions
gptkbp:bfsParent gptkb:Apollo_11_Command_Module
gptkbp:bfsLayer 4