H-IIA 275

GPTKB entity

Statements (114)

Predicate	Object
gptkbp:instance_of	gptkb:Team_Rocket
gptkbp:collaboration	Various international payloads
gptkbp:configuration	275 configuration
gptkbp:debut	over 40 launches
gptkbp:development	Ongoing improvements since inception
gptkbp:diameter	4 meters
gptkbp:engine_type	gptkb:LE-7_A
gptkbp:first_flight	gptkb:2004
gptkbp:height	53 meters
https://www.w3.org/2000/01/rdf-schema#label	H-IIA 275
gptkbp:launch_date	gptkb:2023 August 29, 2004 approximately 2-3 per year
gptkbp:launch_platform	gptkb:JAXA
gptkbp:launch_price	approximately $90 million
gptkbp:launch_site	gptkb:Tanegashima_Space_Center
gptkbp:launch_vehicle	2 or 4 Expendable launch system H-II series
gptkbp:manufacturer	gptkb:Mitsubishi_Heavy_Industries
gptkbp:notable_mission	gptkb:Akasaki gptkb:Hayabusa gptkb:GCOM-W1 gptkb:H-IIA_202
gptkbp:number_of_engines	gptkb:1
gptkbp:number_of_stages	2
gptkbp:operational_period	2004 to present
gptkbp:orbital_altitude	Geostationary transfer orbit
gptkbp:payload_capacity	gptkb:H-IIA_254 gptkb:H-IIA_255 gptkb:H-IIA_265 gptkb:H-IIA_267 gptkb:H-IIA_274 gptkb:H-IIA_251 gptkb:H-IIA_252 gptkb:H-IIA_253 gptkb:H-IIA_256 gptkb:H-IIA_257 gptkb:H-IIA_258 gptkb:H-IIA_260 gptkb:H-IIA_261 gptkb:H-IIA_262 gptkb:H-IIA_263 gptkb:H-IIA_266 gptkb:H-IIA_268 gptkb:H-IIA_269 gptkb:H-IIA_270 gptkb:H-IIA_271 gptkb:H-IIA_272 gptkb:H-IIA_273 gptkb:H-IIA_275 gptkb:GCOM-C gptkb:Quasi-Zenith_Satellite_System gptkb:H-IIA_259 gptkb:H-IIA_264 gptkb:H-IIA_202 gptkb:H-IIA_204 gptkb:H-IIA_205 gptkb:H-IIA_206 gptkb:H-IIA_207 gptkb:H-IIA_208 gptkb:H-IIA_209 gptkb:H-IIA_210 gptkb:H-IIA_211 gptkb:H-IIA_212 gptkb:H-IIA_213 gptkb:H-IIA_214 gptkb:H-IIA_215 gptkb:H-IIA_216 gptkb:H-IIA_217 gptkb:H-IIA_218 gptkb:H-IIA_219 gptkb:H-IIA_220 gptkb:H-IIA_221 gptkb:H-IIA_222 gptkb:H-IIA_223 gptkb:H-IIA_224 gptkb:H-IIA_225 gptkb:H-IIA_226 gptkb:H-IIA_227 gptkb:H-IIA_228 gptkb:H-IIA_229 gptkb:H-IIA_230 gptkb:H-IIA_231 gptkb:H-IIA_232 gptkb:H-IIA_233 gptkb:H-IIA_234 gptkb:H-IIA_235 gptkb:H-IIA_236 gptkb:H-IIA_237 gptkb:H-IIA_238 gptkb:H-IIA_239 gptkb:H-IIA_240 gptkb:H-IIA_241 gptkb:H-IIA_242 gptkb:H-IIA_243 gptkb:H-IIA_244 gptkb:H-IIA_245 gptkb:H-IIA_246 gptkb:H-IIA_247 gptkb:H-IIA_248 gptkb:H-IIA_249 gptkb:H-IIA_250 4 meters in diameter 4,000 kg to geostationary transfer orbit DSN-1
gptkbp:propulsion	Liquid oxygen and kerosene
gptkbp:reliability	high
gptkbp:success_rate	over 90%
gptkbp:successor	gptkb:H-IIB
gptkbp:user	gptkb:Japanese_government Commercial customers
gptkbp:bfsParent	gptkb:JAXA
gptkbp:bfsLayer	4