|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:cargo_capacity
|
up to 6 tons
|
|
gptkbp:cargo_types
|
gptkb:manual
gptkb:ARM
|
|
gptkbp:collaboration
|
gptkb:ESA
gptkb:Roscosmos
gptkb:NASA
|
|
gptkbp:communication_system
|
batteries
solar panels
Ku-band
S-band
|
|
gptkbp:control_system
|
autonomous
|
|
gptkbp:cooling_system
|
active
passive
|
|
gptkbp:crew
|
no
|
|
gptkbp:designed_by
|
gptkb:JAXA
|
|
gptkbp:development
|
gptkb:2005
|
|
gptkbp:docking_system
|
NDS
|
|
gptkbp:durability
|
no
|
|
gptkbp:first_flight
|
gptkb:2009
gptkb:2020
gptkb:HTV-1
gptkb:HTV-9
|
|
gptkbp:flight_style
|
gptkb:9
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
HTV service module
|
|
gptkbp:includes
|
gptkb:power_adapter
unpressurized logistics module
|
|
gptkbp:launch_date
|
annual
|
|
gptkbp:launch_mass
|
16,500 kg
|
|
gptkbp:launch_platform
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:launch_price
|
approximately $30 million
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Team_Rocket
|
|
gptkbp:mass
|
16,500 kg
|
|
gptkbp:mission_type
|
gptkb:scientific_research
cargo resupply
technology demonstration
|
|
gptkbp:module
|
gptkb:logistics
|
|
gptkbp:module_dimensions
|
10.5 m length
4.4 m diameter
|
|
gptkbp:operates_in
|
low Earth orbit
|
|
gptkbp:operational_period
|
2009-2020
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:operational_use
|
gptkb:JAXA
|
|
gptkbp:payload_capacity
|
gptkb:scientific_experiments
gptkb:sports_equipment
gptkb:water
spare parts
food supplies
|
|
gptkbp:payload_delivery_method
|
berthing
unberthing
|
|
gptkbp:primary_function
|
transport cargo to ISS
|
|
gptkbp:production_years
|
gptkb:2008
|
|
gptkbp:safety_features
|
emergency procedures
redundant systems
|
|
gptkbp:service
|
approximately 3 months
|
|
gptkbp:speed
|
no
|
|
gptkbp:successor
|
gptkb:HTV-X
|
|
gptkbp:used_for
|
resupply missions
|
|
gptkbp:bfsParent
|
gptkb:H-II_Transfer_Vehicle_(HTV)
gptkb:H-II_Transfer_Vehicle
|
|
gptkbp:bfsLayer
|
5
|