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gptkbp:instance_of
|
gptkb:Space_Launch_System
gptkb:Team_Rocket
|
|
gptkbp:collaboration
|
JAXA, NASA
|
|
gptkbp:collaborator
|
gptkb:NASA
|
|
gptkbp:configuration
|
two-stage
single configuration
|
|
gptkbp:current_status
|
in service
|
|
gptkbp:design
|
15 years
Mitsubishi Heavy Industries and JAXA
|
|
gptkbp:development
|
5 years
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:diameter
|
4 meters
|
|
gptkbp:engine_configuration
|
staged combustion cycle
|
|
gptkbp:engine_type
|
gptkb:LE-7_A
LE-7 A and LE-5 B
|
|
gptkbp:first_flight
|
gptkb:2009
2009-09-10
2020-11-24
September 10, 2009
|
|
gptkbp:flight_style
|
gptkb:5
|
|
gptkbp:fuel_type
|
Liquid oxygen and kerosene
|
|
gptkbp:height
|
53 meters
56 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-IIB
|
|
gptkbp:inspiration
|
gptkb:H-IIA
|
|
gptkbp:launch_date
|
1-2 per year
approximately 1 per year
|
|
gptkbp:launch_mass
|
200 tons
|
|
gptkbp:launch_platform
|
gptkb:Tanegashima_Space_Center
gptkb:JAXA
|
|
gptkbp:launch_price
|
$150 million
approximately $150 million
|
|
gptkbp:launch_site
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:H-IIA
gptkb:Launch_Complex_2
expendable launch vehicle
H-II family
|
|
gptkbp:launch_window
|
varies
|
|
gptkbp:launched
|
8
|
|
gptkbp:launches_to_geostationary_orbit
|
2
|
|
gptkbp:launches_to_international_space_station
|
gptkb:6
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:mission_type
|
cargo delivery
|
|
gptkbp:notable_launches
|
gptkb:HTV-1
|
|
gptkbp:notable_mission
|
HTV-1 to HTV-8
|
|
gptkbp:number_of_engines
|
gptkb:4
|
|
gptkbp:number_of_stages
|
gptkb:solid_rocket_boosters
2
2 stages
liquid-fueled engine
|
|
gptkbp:operated_by
|
gptkb:JAXA
|
|
gptkbp:operational_period
|
11 years
|
|
gptkbp:operational_status
|
operational
retired
|
|
gptkbp:payload_capacity
|
4.0 meters
16,000 kg
8,000 kg
16 tons
5 meters in diameter
10.0 meters
various satellites and cargo
16,500 kg to low Earth orbit
16 tons to low Earth orbit
|
|
gptkbp:primary_use
|
cargo resupply missions
|
|
gptkbp:production_status
|
mature
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:reliability
|
high
high reliability
|
|
gptkbp:strategic_goals
|
gptkb:0
|
|
gptkbp:success
|
8
|
|
gptkbp:success_rate
|
100%
over 90%
|
|
gptkbp:successor
|
gptkb:H-IIB_Block_2
|
|
gptkbp:technology
|
gptkb:advanced_propulsion_systems
|
|
gptkbp:used_for
|
gptkb:HTV_cargo_missions
gptkb:HTV_missions
|
|
gptkbp:bfsParent
|
gptkb:Tanegashima_Space_Center
gptkb:JAXA
gptkb:Japanese_Aerospace_Exploration_Agency
gptkb:Japan_Aerospace_Exploration_Agency
gptkb:Japanese_Aerospace_Exploration_Agency_(JAXA)
gptkb:Japan_Aerospace_Exploration_Agency_(JAXA)
|
|
gptkbp:bfsLayer
|
4
|