|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Space_X_missions
|
|
gptkbp:check_in_time
|
5 seconds
|
|
gptkbp:controls
|
gptkb:battle
computer controlled
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:debut_year
|
gptkb:2014
|
|
gptkbp:designed_by
|
gptkb:Space_X
|
|
gptkbp:developer
|
$100 million
|
|
gptkbp:emissions_standard
|
converging-diverging
|
|
gptkbp:engine
|
gptkb:2010
gptkb:2014
gptkb:2015
8
high
controlled
staged combustion
high thrust-to-weight ratio
Crew Dragon missions
instantaneous
replaced by newer systems
gimbal-mounted
development testing
|
|
gptkbp:first_flight
|
gptkb:2015
|
|
gptkbp:fuel_capacity
|
0.5 m
1.5 m
|
|
gptkbp:fuel_type
|
RP-1 and liquid oxygen
kerosene
Inconel
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Super Draco engine
|
|
gptkbp:ignition_system
|
hypergolic ignition
|
|
gptkbp:is_tested_for
|
gptkb:Mc_Gregor,_Texas
Space X Rocket Development and Test Facility
|
|
gptkbp:launch_vehicle
|
gptkb:battle
|
|
gptkbp:launched
|
gptkb:battle
|
|
gptkbp:legal_issue
|
staged combustion cycle
|
|
gptkbp:manufacturer
|
gptkb:Space_X
|
|
gptkbp:max_speed
|
330 seconds
|
|
gptkbp:number_of_rooms
|
1,000 psi
|
|
gptkbp:operational_area
|
crew safety
|
|
gptkbp:propulsion
|
16,000 lbf
178:1
|
|
gptkbp:purpose
|
gptkb:aircraft
|
|
gptkbp:related_to
|
gptkb:spacecraft
|
|
gptkbp:safety_features
|
launch escape capability
|
|
gptkbp:social_structure
|
liquid oxygen
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Draco_engine
|
|
gptkbp:type
|
gptkb:rocket
|
|
gptkbp:used_in
|
gptkb:Dragon_spacecraft
|
|
gptkbp:valve_configuration
|
solenoid valves
|
|
gptkbp:weight
|
90 lb
|