|
gptkbp:instance_of
|
gptkb:ship
|
|
gptkbp:cargo_capacity
|
6,000 kg
|
|
gptkbp:cargo_return_capability
|
yes
|
|
gptkbp:cargo_transfer_duration
|
up to 2 weeks
|
|
gptkbp:cargo_types
|
gptkb:ARM
food, equipment, experiments
|
|
gptkbp:collaboration
|
yes
NASA, ESA, Roscosmos
|
|
gptkbp:communication_system
|
S-band, Ku-band
|
|
gptkbp:control_system
|
autonomous
|
|
gptkbp:crew
|
limited
|
|
gptkbp:debut
|
2008-2020
|
|
gptkbp:decommissioned
|
gptkb:2020
|
|
gptkbp:deorbit_capability
|
yes
|
|
gptkbp:design
|
3 years
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:diameter
|
4.4 m
|
|
gptkbp:docking_system
|
NDS
|
|
gptkbp:durability
|
no
|
|
gptkbp:first_flight
|
gptkb:HTV-9
September 10, 2008
|
|
gptkbp:flight_style
|
gptkb:9
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Japanese HTV
|
|
gptkbp:investment
|
yes
|
|
gptkbp:launch_date
|
annual
|
|
gptkbp:launch_event
|
100%
|
|
gptkbp:launch_mass
|
up to 16,500 kg
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Team_Rocket
H-IIA, H-IIB
|
|
gptkbp:length
|
9.8 m
|
|
gptkbp:manufacturer
|
gptkb:JAXA
|
|
gptkbp:mass
|
16,500 kg
|
|
gptkbp:mission
|
gptkb:HTV-1
9 missions
HTV-9 in May 2020
|
|
gptkbp:mission_duration
|
up to 30 days
|
|
gptkbp:operates_in
|
gptkb:2020
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:orbital_altitude
|
400 km
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:payload_capacity
|
gptkb:JAXA
yes
pressurized, unpressurized
|
|
gptkbp:purpose
|
resupply the International Space Station
|
|
gptkbp:safety_features
|
multiple redundancy
|
|
gptkbp:scientific_payloads
|
yes
|
|
gptkbp:spacecraft
|
modular
uncrewed
|
|
gptkbp:speed
|
yes
|
|
gptkbp:successor
|
gptkb:HTV-X
|
|
gptkbp:sustainability
|
yes
|
|
gptkbp:was_a_demonstration_of
|
yes
|
|
gptkbp:bfsParent
|
gptkb:International_Space_Station
|
|
gptkbp:bfsLayer
|
4
|