|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:collaboration
|
gptkb:NASA
|
|
gptkbp:configuration
|
two-stage
|
|
gptkbp:control_system
|
Inertial navigation system
|
|
gptkbp:debut
|
successful missions
|
|
gptkbp:design_purpose
|
heavy-lift launch vehicle
|
|
gptkbp:development
|
gptkb:2006
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:durability
|
no
|
|
gptkbp:engine_configuration
|
staged combustion cycle
|
|
gptkbp:engine_type
|
gptkb:LE-7_A
|
|
gptkbp:final_flight_year
|
gptkb:2020
|
|
gptkbp:first_flight
|
2009-09-10
2020-11-24
|
|
gptkbp:fuel_type
|
RP-1 and Liquid Oxygen
|
|
gptkbp:guidance_system
|
gptkb:GPS
|
|
gptkbp:height
|
53 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIB rocket
|
|
gptkbp:launch_date
|
annual
|
|
gptkbp:launch_event
|
gptkb:0
8
|
|
gptkbp:launch_mass
|
200 tons
|
|
gptkbp:launch_platform
|
gptkb:JAXA
JAXA control center
|
|
gptkbp:launch_price
|
$150 million
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:launch_vehicle
|
2
expendable launch vehicle
H-II
|
|
gptkbp:launched
|
gptkb:Launch_Complex_2
8
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:mission
|
successful deployment
vertical ascent
|
|
gptkbp:mission_duration
|
varies by payload
|
|
gptkbp:number_of_engines
|
gptkb:4
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operational_period
|
2009 to 2020
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:payload_capacity
|
5 meters
8 tons
16 tons
orbital insertion
|
|
gptkbp:primary_mission
|
International Space Station resupply
Satellite deployment
|
|
gptkbp:propulsion
|
50:1
1,000 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:success_rate
|
100%
|
|
gptkbp:used_for
|
gptkb:HTV_missions
|
|
gptkbp:bfsParent
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:bfsLayer
|
4
|