|
gptkbp:instance_of
|
gptkb:power_adapter
|
|
gptkbp:associated_with
|
gptkb:International_Space_Station
|
|
gptkbp:capacity
|
up to 3,500 kg of cargo
|
|
gptkbp:cargo_types
|
varies by mission
food, equipment, experiments
can return cargo to Earth
|
|
gptkbp:collaboration
|
NASA and Northrop Grumman
|
|
gptkbp:communication_system
|
S-band and Ku-band
|
|
gptkbp:crew
|
gptkb:none
designed with crew safety in mind
|
|
gptkbp:data_return
|
yes
|
|
gptkbp:debut
|
gptkb:2016
multiple successful missions
|
|
gptkbp:designed_by
|
gptkb:Northrop_Grumman
|
|
gptkbp:dimensions
|
4.5 m in diameter
|
|
gptkbp:discovery_year
|
controlled reentry
|
|
gptkbp:docking_system
|
gptkb:Common_Berthing_Mechanism
|
|
gptkbp:durability
|
not reusable
|
|
gptkbp:environmental_concerns
|
temperature and humidity regulation
|
|
gptkbp:features
|
automated cargo delivery
|
|
gptkbp:future_plans
|
upgrades for next generation missions
|
|
gptkbp:has_limitations
|
limited by ISS docking schedule
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Cygnus pressurized module
|
|
gptkbp:launch_date
|
approximately twice a year
|
|
gptkbp:launch_event
|
high success rate
|
|
gptkbp:launch_platform
|
gptkb:Northrop_Grumman
|
|
gptkbp:launch_site
|
gptkb:Wallops_Flight_Facility
|
|
gptkbp:launch_vehicle
|
gptkb:Antares_rocket
|
|
gptkbp:launch_window
|
scheduled based on ISS needs
|
|
gptkbp:manufacturer
|
gptkb:Northrop_Grumman_Innovation_Systems
|
|
gptkbp:mass
|
approximately 3,000 kg
|
|
gptkbp:mission
|
gptkb:Orb-1
support ISS operations
NG-16
|
|
gptkbp:mission_duration
|
up to 90 days
|
|
gptkbp:module
|
uncrewed spacecraft
|
|
gptkbp:operates_in
|
low Earth orbit
|
|
gptkbp:operational_since
|
gptkb:2016
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:operational_use
|
gptkb:ground
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:orbital_period
|
approximately 90 minutes
|
|
gptkbp:part_of
|
Commercial Resupply Services program
|
|
gptkbp:partnerships
|
collaborates with various space agencies
|
|
gptkbp:payload_capacity
|
gptkb:scientific_experiments
up to 3,500 kg
3,500 kg
pre-launch at Wallops
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:related_vehicle
|
designed for safe reentry
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:spacecraft
|
automated cargo spacecraft
|
|
gptkbp:successor
|
gptkb:Cygnus_NG-20
|
|
gptkbp:supply_chain
|
supports ISS supply chain
|
|
gptkbp:sustainability
|
designed for minimal environmental impact
|
|
gptkbp:used_for
|
cargo resupply missions
|
|
gptkbp:was_a_demonstration_of
|
supports technology demonstrations
|
|
gptkbp:bfsParent
|
gptkb:Cygnus_CRS_OA-3
gptkb:Cygnus_CRS_Orb-4
|
|
gptkbp:bfsLayer
|
6
|