H-IIA 202 series

GPTKB entity

Statements (52)
Predicate Object
gptkbp:instance_of gptkb:Team_Rocket
gptkbp:challenges overcome during development
gptkbp:collaboration with NASA
gptkbp:configuration two-stage
H-IIA 202, H-IIA 204
gptkbp:debut multiple successful launches
gptkbp:design 15 years
gptkbp:design_features modular design
gptkbp:diameter 4 meters
gptkbp:durability gptkb:none
gptkbp:engine_type liquid-fueled
gptkbp:environmental_impact assessed by JAXA
gptkbp:failure_launches gptkb:1
gptkbp:first_flight 2004-02-20
gptkbp:fuel_type RP-1 and liquid oxygen
gptkbp:future_prospects influence on new designs
gptkbp:guidance_system inertial navigation
gptkbp:height 53 meters
https://www.w3.org/2000/01/rdf-schema#label H-IIA 202 series
gptkbp:influences future Japanese launch vehicles
gptkbp:launch_date annual
gptkbp:launch_platform gptkb:ground
Japan Aerospace Exploration Agency (JAXA
gptkbp:launch_price $90 million
gptkbp:launch_site gptkb:Tanegashima_Space_Center
gptkbp:launch_statistics available on spaceflight databases
gptkbp:launch_vehicle H-II family
gptkbp:launch_window varies
gptkbp:legacy successor to H-IIA 201 series
gptkbp:manufacturer gptkb:Mitsubishi_Heavy_Industries
gptkbp:media_coverage extensive during operational years
gptkbp:mission decommissioned
gptkbp:notable_launches H-IIA 202 launch of Akasaki satellite
gptkbp:number_of_engines 2
gptkbp:number_of_stages gptkb:HM-7_B
gptkb:LE-7_A
gptkbp:operational_period 2004-2020
gptkbp:operational_status retired
gptkbp:payload_capacity 4 meters
1,500 kg
4,000 kg
vertical integration
gptkbp:primary_mission satellite deployment
gptkbp:propulsion 1,000 k N
gptkbp:public_interest high in Japan
gptkbp:reliability high
gptkbp:safety_record excellent
gptkbp:specification available on JAXA website
gptkbp:success gptkb:30
gptkbp:success_rate 98%
gptkbp:bfsParent gptkb:H-IIA_292_rocket
gptkbp:bfsLayer 5