|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
3
|
|
gptkbp:bfsParent
|
gptkb:spacecraft
|
|
gptkbp:application
|
crew safety
|
|
gptkbp:check_in_time
|
5 seconds
|
|
gptkbp:controls
|
computer controlled
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:design
|
modular
|
|
gptkbp:designed_by
|
Space X engineers
|
|
gptkbp:developer
|
gptkb:significant
ongoing
|
|
gptkbp:emergency_services
|
gptkb:battle
crew escape
|
|
gptkbp:engine
|
8
completed
staged combustion
proven
clustered
optimized for safety
|
|
gptkbp:first_flight
|
gptkb:2010
multiple
|
|
gptkbp:first_introduced
|
gptkb:Crew_Dragon_Demo-1
|
|
gptkbp:fuel_capacity
|
high
3.5 ft
6.5 ft
|
|
gptkbp:fuel_type
|
hypergolic
monomethylhydrazine (MMH)
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Super Draco
|
|
gptkbp:ignition_system
|
hypergolic ignition
|
|
gptkbp:influenced_by
|
previous rocket engines
|
|
gptkbp:inspired_by
|
gptkb:Apollo_launch_escape_system
|
|
gptkbp:integrates_with
|
gptkb:Dragon_2_spacecraft
|
|
gptkbp:is_designed_for
|
gptkb:spacecraft
|
|
gptkbp:is_tested_for
|
static fire tests
Space X facilities
|
|
gptkbp:is_used_for
|
crew safety during launch
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:launch_vehicle
|
gptkb:battle
|
|
gptkbp:manufacturer
|
gptkb:Space_X
|
|
gptkbp:mission
|
gptkb:Commercial_Crew_Program
|
|
gptkbp:operated_by
|
gptkb:NASA
|
|
gptkbp:operational_status
|
gptkb:2019
active
|
|
gptkbp:part_of
|
gptkb:Crew_Dragon_system
|
|
gptkbp:performance
|
high thrust-to-weight ratio
|
|
gptkbp:propulsion
|
gptkb:Dragon_2
gptkb:battle
up to 16,000 lbf
16,000 lbf
|
|
gptkbp:purpose
|
gptkb:aircraft
|
|
gptkbp:reliability
|
high
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:safety_record
|
excellent
|
|
gptkbp:social_structure
|
gptkb:dinitrogen_tetroxide
nitrogen tetroxide (N2 O4)
|
|
gptkbp:technology
|
gptkb:bird
|
|
gptkbp:type
|
hypergolic engine
|
|
gptkbp:used_in
|
gptkb:Dragon_spacecraft
|
|
gptkbp:weight
|
1,200 lb
|