Statements (94)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:academic_programs |
Experienced engineering team involved
|
| gptkbp:community_engagement |
Public engagement initiatives undertaken
|
| gptkbp:community_outreach |
Educational outreach programs implemented
|
| gptkbp:configuration |
gptkb:H-IIA_202
H-IIA 202 configuration |
| gptkbp:control_system |
Digital control system
digital control system |
| gptkbp:debut |
2004 to 2020
Part of H-IIA launch history |
| gptkbp:development |
H-IIA program
|
| gptkbp:diameter |
4 meters
|
| gptkbp:engine_type |
gptkb:LE-7_A
LE-7 A engine |
| gptkbp:environmental_impact |
Environmental impact assessments conducted
|
| gptkbp:first_flight |
gptkb:2001
gptkb:2004 gptkb:2019 gptkb:2020 |
| gptkbp:fuel_type |
Liquid hydrogen and liquid oxygen
|
| gptkbp:guidance_system |
gptkb:navigation_system
Inertial guidance system |
| gptkbp:healthcare |
Advanced telemetry system
|
| gptkbp:height |
53 meters
|
| gptkbp:history |
Developed in the 1990s
|
| https://www.w3.org/2000/01/rdf-schema#label |
H-IIA 216
|
| gptkbp:launch_date |
annual
2004-2009 2019-11-30 2019-01-18 Regular launch frequency |
| gptkbp:launch_documentation |
Comprehensive launch documentation available
|
| gptkbp:launch_event |
High success rate
|
| gptkbp:launch_operator |
gptkb:Japan_Aerospace_Exploration_Agency
|
| gptkbp:launch_platform |
Japan Aerospace Exploration Agency (JAXA
Post-launch support provided Remote launch control |
| gptkbp:launch_price |
Approximately $100 million
|
| gptkbp:launch_site |
gptkb:Tanegashima_Space_Center
|
| gptkbp:launch_vehicle |
gptkb:H-IIA
gptkb:H-IIA_family gptkb:H-IIA_202 2 expendable launch vehicle Expendable launch vehicle medium-lift Optional solid rocket boosters |
| gptkbp:launch_window |
Specific launch windows required
|
| gptkbp:launched |
gptkb:Akasaki_satellite
38 multiple |
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:mission |
Successful
Post-mission analysis conducted Standard mission profile |
| gptkbp:mission_type |
gptkb:Space_Launch_System
Satellite launch |
| gptkbp:notable_launches |
H-IIA 216 launch of Akasaki satellite
|
| gptkbp:notable_mission |
communications satellites
|
| gptkbp:number_of_stages |
2 stages
|
| gptkbp:operational_period |
15 years of operation
|
| gptkbp:operational_status |
Retired
retired |
| gptkbp:operator |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:orbit_type |
Sun-synchronous orbit
|
| gptkbp:payload_capacity |
gptkb:Akasaki_satellite
gptkb:DAICHI-2 4 meters in diameter 10,000 kg to geostationary transfer orbit 4,000 kg to geostationary transfer orbit Multiple payload options available Payload integration services offered |
| gptkbp:primary_mission |
Satellite deployment
|
| gptkbp:project |
Effective project management practices
Future developments planned for successors |
| gptkbp:propulsion |
1,000 k N
|
| gptkbp:regulatory_compliance |
Compliance with regulatory standards
|
| gptkbp:release_country |
Conducted international launches
|
| gptkbp:reliability |
High reliability
very reliable |
| gptkbp:safety_measures |
Strict safety protocols followed
|
| gptkbp:stakeholders |
Engagement with stakeholders throughout development
|
| gptkbp:success |
gptkb:true
multiple successful launches |
| gptkbp:success_rate |
high
98% |
| gptkbp:supports |
Specialized ground support equipment used
|
| gptkbp:track |
Tracking system for launches
|
| gptkbp:weather_constraints |
Weather constraints considered
|
| gptkbp:bfsParent |
gptkb:JAXA
gptkb:Japanese_Aerospace_Exploration_Agency gptkb:Japanese_Aerospace_Exploration_Agency_(JAXA) gptkb:Japan_Aerospace_Exploration_Agency_(JAXA) |
| gptkbp:bfsLayer |
4
|