LE-7 A-1

GPTKB entity

Statements (84)

Predicate	Object
gptkbp:instance_of	gptkb:rocket
gptkbp:bfsLayer	4
gptkbp:bfsParent	gptkb:LE-7_A
gptkbp:application	gptkb:spacecraft
gptkbp:check_in_time	approximately 500 seconds
gptkbp:controls	digital control system
gptkbp:cooling_system	regenerative cooling
gptkbp:developed_by	gptkb:Mitsubishi_Heavy_Industries
gptkbp:developer	gptkb:1980 gptkb:1994
gptkbp:emissions_standard	bell nozzle
gptkbp:engine	2 staged combustion two engines
gptkbp:engine_type	gptkb:rocket
gptkbp:first_flight	gptkb:television_series gptkb:1994 gptkb:2009
gptkbp:fuel_type	liquid hydrogen and liquid oxygen
https://www.w3.org/2000/01/rdf-schema#label	LE-7 A-1
gptkbp:launch_site	gptkb:Tanegashima_Space_Center
gptkbp:launched	H-IIA and H-IIB missions
gptkbp:manufacturer	gptkb:Mitsubishi_Heavy_Industries
gptkbp:mission	geostationary transfer orbit
gptkbp:notable_album	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 H-IIA 203 H-IIB 201 H-IIB 202
gptkbp:number_of_rooms	single chamber 20 M Pa
gptkbp:operational_status	retired
gptkbp:propulsion	450 seconds 1,000 k N
gptkbp:reliability	high reliability
gptkbp:successor	LE-7 A-2
gptkbp:used_in	gptkb:H-II_rocket
gptkbp:weight	3,000 kg