|
gptkbp:instanceOf
|
gptkb:satellite
|
|
gptkbp:book
|
gptkb:LE-5A
|
|
gptkbp:cause
|
first stage engine failure (on some flights)
|
|
gptkbp:costPerLaunch
|
~$190 million (1990s USD)
|
|
gptkbp:countryOfOrigin
|
gptkb:Japan
|
|
gptkbp:developedBy
|
gptkb:NASDA
|
|
gptkbp:diameter
|
4.0 m
|
|
gptkbp:firstFlight
|
1994-02-03
|
|
gptkbp:flightNumber
|
7
|
|
gptkbp:height
|
49.0 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
H-II rocket
|
|
gptkbp:lastFlight
|
1999-11-15
|
|
gptkbp:launchSite
|
gptkb:Tanegashima_Space_Center
|
|
gptkbp:manufacturer
|
gptkb:Mitsubishi_Heavy_Industries
|
|
gptkbp:mass
|
260,000 kg
|
|
gptkbp:notableMission
|
gptkb:ADEOS_I
gptkb:COMETS
gptkb:ETS-VI
gptkb:Kakehashi
|
|
gptkbp:numberOfFailedFlights
|
2
|
|
gptkbp:numberOfStages
|
gptkb:LE-7
2
|
|
gptkbp:numberOfSuccessfulFlights
|
5
|
|
gptkbp:operator
|
gptkb:NASDA
|
|
gptkbp:payloadToGTO
|
4,000 kg
|
|
gptkbp:payloadToLEO
|
10,000 kg
|
|
gptkbp:propulsion
|
liquid oxygen
liquid hydrogen
|
|
gptkbp:replacedBy
|
gptkb:H-I_rocket
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:H-IIA_rocket
|
|
gptkbp:usedFor
|
gptkb:technology
satellite launches
|
|
gptkbp:bfsParent
|
gptkb:H-IIA_rocket
gptkb:National_Space_Development_Agency_of_Japan
|
|
gptkbp:bfsLayer
|
6
|