|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:air_traffic_control
|
manual and automated systems
|
|
gptkbp:challenges
|
weight reduction
|
|
gptkbp:communication_system
|
S-band radio
|
|
gptkbp:components
|
gptkb:spacecraft
|
|
gptkbp:contributed_to
|
advancements in space technology
|
|
gptkbp:control_surfaces
|
reaction control thrusters
|
|
gptkbp:control_system
|
manual and automatic
fly-by-wire system
|
|
gptkbp:cooling_system
|
ablative heat shield
Phenolic resin
|
|
gptkbp:crew
|
yes
high priority
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:design
|
14 days
NASA engineers
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:development
|
3 years
|
|
gptkbp:diameter
|
3.9 meters
|
|
gptkbp:emergency_services
|
yes
|
|
gptkbp:first_flight
|
gptkb:Apollo_5
gptkb:Apollo_1
|
|
gptkbp:fuel_type
|
liquid oxygen and hydrogen
|
|
gptkbp:has_limitations
|
limited to low Earth orbit
|
|
gptkbp:historical_context
|
gptkb:Cold_War_space_race
|
|
gptkbp:historical_significance
|
first crewed spacecraft for Apollo missions
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Block I Command Module
|
|
gptkbp:influenced
|
modern spacecraft design
|
|
gptkbp:influenced_by
|
previous spacecraft designs
|
|
gptkbp:inspiration
|
future spacecraft designs
|
|
gptkbp:inspired
|
future generations of astronauts.
|
|
gptkbp:instruments
|
gptkb:sports_equipment
|
|
gptkbp:involved_in
|
Apollo 1 accident investigation
testing of lunar landing technologies
|
|
gptkbp:is_tested_for
|
extensive ground testing
|
|
gptkbp:landing_distance
|
three main parachutes
|
|
gptkbp:last_successful_mission
|
gptkb:Apollo_5
|
|
gptkbp:launch_date
|
1966-02-26
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Saturn_IB
|
|
gptkbp:legacy
|
paved the way for Apollo missions
|
|
gptkbp:length
|
3.9 meters
|
|
gptkbp:life_support_system
|
yes
|
|
gptkbp:manufacturer
|
gptkb:North_American_Aviation
|
|
gptkbp:mass
|
5,000 kg
|
|
gptkbp:mission
|
gptkb:Apollo_5
gptkb:Apollo_4
conducted for improvements
|
|
gptkbp:mission_type
|
manned spaceflight
|
|
gptkbp:navigation_system
|
gptkb:navigation_system
|
|
gptkbp:notable_features
|
modular design
|
|
gptkbp:operational_period
|
1966-1968
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:operational_use
|
command and service module
|
|
gptkbp:orbital_altitude
|
yes
|
|
gptkbp:part_of
|
gptkb:NASA's_human_spaceflight_program
|
|
gptkbp:power_source
|
fuel cells
|
|
gptkbp:primary_function
|
crew transport
|
|
gptkbp:recovery_method
|
ocean recovery
|
|
gptkbp:safety_features
|
multiple redundancies
|
|
gptkbp:speed
|
yes
|
|
gptkbp:successor
|
gptkb:Block_II_Command_Module
|
|
gptkbp:used_in
|
gptkb:Apollo_program
|
|
gptkbp:bfsParent
|
gptkb:Apollo_1
|
|
gptkbp:bfsLayer
|
5
|