|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Expedition_72
|
|
gptkbp:aircraft_operated
|
Autonomous
|
|
gptkbp:collaborations
|
gptkb:NASA
|
|
gptkbp:communication
|
S-band and Ku-band
|
|
gptkbp:cooling_system
|
Passive and active
|
|
gptkbp:crew
|
gptkb:0
Not applicable
|
|
gptkbp:date
|
2016-03-18
|
|
gptkbp:design
|
gptkb:NASA
|
|
gptkbp:dimensions
|
3.7 m diameter
|
|
gptkbp:durability
|
gptkb:battle
|
|
gptkbp:events
|
100%
|
|
gptkbp:first_flight
|
gptkb:CRS-10
Low Earth Orbit
2017-03-07
2012-10-08
|
|
gptkbp:home_port
|
gptkb:International_Docking_System_Standard
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Dragon CRS-100
|
|
gptkbp:is_a_destination_for
|
gptkb:International_Space_Station
|
|
gptkbp:launch_date
|
2016-02-19
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral_Air_Force_Station
gptkb:Space_X
|
|
gptkbp:launch_vehicle
|
gptkb:Falcon_9
4,200 kg
|
|
gptkbp:launched
|
gptkb:Open
|
|
gptkbp:manufacturer
|
gptkb:Space_X
|
|
gptkbp:mass
|
3,000 kg
4,000 kg
|
|
gptkbp:max_takeoff_weight
|
gptkb:Parachutes
|
|
gptkbp:mission
|
gptkb:Space_X_Mission_Control
Successful
Conducted
Cargo resupply mission
|
|
gptkbp:mission_duration
|
approximately 28 days
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:orbital_period
|
90 minutes
|
|
gptkbp:power_output
|
Solar panels
|
|
gptkbp:propulsion
|
gptkb:Draco_thrusters
|
|
gptkbp:safety_features
|
Redundant systems
|
|
gptkbp:seating_capacity
|
gptkb:physicist
gptkb:ISS
Experiments
6,000 kg
3,500 kg
Scientific equipment
Supplies for ISS
|
|
gptkbp:speed
|
Heat shield
|
|
gptkbp:status
|
Completed
|
|
gptkbp:succeeded_by
|
gptkb:theorem
|