Statements (73)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
gptkb:rocket |
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:JAXA
|
| gptkbp:collaborations |
gptkb:battle
|
| gptkbp:country |
Japan and international clients
|
| gptkbp:customer_support |
Comprehensive support offered
|
| gptkbp:debut_year |
gptkb:2021
Multiple successful launches |
| gptkbp:diameter |
4 meters
|
| gptkbp:engine |
gptkb:musical
|
| gptkbp:engine_type |
gptkb:LE-7_A
gptkb:item |
| gptkbp:environmental_impact |
Minimized emissions
|
| gptkbp:first_flight |
gptkb:2001
gptkb:2004 2021-03-30 2004-08-29 |
| gptkbp:future_plans |
Continued use for satellite launches
|
| gptkbp:guidance_system |
Inertial navigation system
|
| gptkbp:height |
53 meters
|
| gptkbp:home_ground |
Extensive ground testing conducted
|
| https://www.w3.org/2000/01/rdf-schema#label |
H-IIA 264
|
| gptkbp:innovation |
Continuous improvements made
|
| gptkbp:launch_date |
gptkb:Regular
|
| gptkbp:launch_site |
gptkb:Tanegashima_Space_Center
Japan Aerospace Exploration Agency (JAXA Over 40 launches Automated launch control system Conducted for each mission Detailed documentation provided |
| gptkbp:launch_vehicle |
Expendable launch vehicle
H-II family Two-stage design |
| gptkbp:launched |
gptkb:Akasaki_satellite
Several months Ground support equipment Varies by mission |
| gptkbp:manufacturer |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:market |
Approximately $90 million
|
| gptkbp:mission |
gptkb:JAXA_Mission_Control_Center
High success rate |
| gptkbp:mission_duration |
Varies by mission
|
| gptkbp:notable_achievement |
Successful deployment of multiple satellites
|
| gptkbp:notable_album |
H-IIA 264 launched Akasaki satellite
|
| gptkbp:number_of_stages |
gptkb:Solid_Rocket_Boosters
gptkb:LE-5_A_engine 2 |
| gptkbp:operational_status |
Active
|
| gptkbp:orbital_inclination |
Geostationary orbit
|
| gptkbp:partnerships |
Collaborations with various space agencies
|
| gptkbp:produced_by |
Operational
|
| gptkbp:propulsion |
RP-1 and Liquid Oxygen
|
| gptkbp:purpose |
Satellite launch
|
| gptkbp:reliability |
Proven
|
| gptkbp:safety_record |
Good safety record
|
| gptkbp:seating_capacity |
10,000 kg
4,000 kg Composite material 10,000 kg to geostationary transfer orbit Multiple configurations available 4,000 kg to geostationary transfer orbit Pre-launch integration at Tanegashima Precise deployment capabilities |
| gptkbp:services |
gptkb:Mitsubishi_Heavy_Industries
|
| gptkbp:setting |
gptkb:H-IIA_202
|
| gptkbp:specifies |
Detailed specifications available
|
| gptkbp:succeeded_by |
gptkb:High
95% over 90% |
| gptkbp:technology |
Provided to international clients
|
| gptkbp:training |
Available for clients
|
| gptkbp:upgrades |
Planned upgrades for enhanced performance
|