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DBpedia 2014

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M-V diameter "2.5".
M-V height "30800.0".
M-V lowerEarthOrbitPayload "1800.0".
M-V abstract "The M-V rocket, also called M-5 or Mu-5, was a Japanese solid-fuel rocket designed to launch scientific satellites. It was a member of the Mu family of rockets. The Institute of Space and Astronautical Science (ISAS) began developing the M-V in 1990 at a cost of 15 billion yen. It has three stages and is 30.7 meters high, 2.5 meters in diameter, and weighs about 140 tonnes (310,000 pounds). It was capable of launching a satellite weighing 1.8 tonnes (2 short tons) into an orbit as high as 250 km (160 mi).The first M-V rocket launched the HALCA radio astronomy satellite in 1997, and the second the Nozomi Mars explorer in July 1998. The third rocket attempted to launch the Astro-E X-ray satellite on February 10, 2000 but failed.ISAS recovered from this setback and launched Hayabusa to 25143 Itokawa in 2003.The following M-V launch was the scientific Astro-E2 satellite, a replacement for Astro-E, which took place on July 10, 2005.The final launch was that of the Hinode (SOLAR-B) spacecraft, along with the SSSat microsat and a nanosatellite, HIT-SAT, on 22 September 2006.".
M-V countryOrigin Japan.
M-V diameter "2.5".
M-V failedLaunches "1".
M-V finalFlight "2003-05-09".
M-V finalFlight "2006-09-22".
M-V height "30.8".
M-V launchSite Kagoshima.
M-V lowerEarthOrbitPayload "1800000.0".
M-V maidenFlight "1997-02-12".
M-V maidenFlight "2000-02-10".
M-V manufacturer Nissan_Motor_Company.
M-V rocketFunction Solid-fuel_rocket.
M-V rocketStages "3".
M-V rocketStages "4".
M-V status "Retired".
M-V successfulLaunches "6".
M-V thumbnail M-V_launching_ASTRO-E2.jpeg?width=300.
M-V totalLaunches "7".
M-V wikiPageExternalLink mv.htm.
M-V wikiPageExternalLink index.shtml.
M-V wikiPageExternalLink index.shtml.
M-V wikiPageExternalLink index_e.html.
M-V wikiPageExternalLink index_e.html.
M-V wikiPageID "866654".
M-V wikiPageRevisionID "575724697".
M-V altDiameter "8.2".
M-V altHeight "101.0".
M-V altLeo "3900.0".
M-V altMass "303100".
M-V altPayload "2800.0".
M-V altStage1thrust "849855".
M-V altStage2thrust "279952".
M-V altStage3thrust "66093".
M-V altStage4thrust "11668".
M-V caption "The fifth M-V launches with the ASTRO-EII spacecraft.".
M-V countryOrigin Japan.
M-V diameter "2.5 m".
M-V fail "1".
M-V first "--02-10".
M-V first "--02-12".
M-V function "All-solid small orbital launch vehicle".
M-V hasPhotoCollection M-V.
M-V height "30.8 m".
M-V last "--05-09".
M-V last "--09-22".
M-V launches "7".
M-V leoPayload "1800.0".
M-V manufacturer Nissan_Motor_Company.
M-V manufacturer "IHI AEROSPACE".
M-V mass "137500".
M-V name "M-V".
M-V payload "1300.0".
M-V payloadLocation Low_Earth_orbit.
M-V payloadLocation Polar_orbit.
M-V payloads Akari_(satellite).
M-V payloads HALCA.
M-V payloads Hayabusa.
M-V payloads Hinode.
M-V payloads Nozomi_(spacecraft).
M-V payloads Suzaku_(satellite).
M-V sites Kagoshima.
M-V stage1engines "1".
M-V stage1fuel Solid-fuel_rocket.
M-V stage1name M-14_(rocket).
M-V stage1si "246.0".
M-V stage1thrust "3,780.345 kN".
M-V stage1time "46.0".
M-V stage2engines "1".
M-V stage2fuel Solid-fuel_rocket.
M-V stage2name M-24_(rocket).
M-V stage2si "203.0".
M-V stage2thrust "1,245.287 kN".
M-V stage2time "71.0".
M-V stage3engines "1".
M-V stage3fuel Solid-fuel_rocket.
M-V stage3name M-34_(rocket).
M-V stage3si "301.0".
M-V stage3thrust "294 kN".
M-V stage3time "102.0".
M-V stage4diff "M-V KM".
M-V stage4engines "1".
M-V stage4fuel Solid-fuel_rocket.
M-V stage4name KM-V1.
M-V stage4si "298.0".
M-V stage4thrust "51.9 kN".
M-V stage4time "73.0".
M-V stages "3".
M-V status "Retired".
M-V success "6".
M-V subject Category:Solid-fuel_rockets.
M-V subject Category:Space_launch_vehicles_of_Japan.
M-V type Artifact100021939.
M-V type Conveyance103100490.
M-V type Instrumentality103575240.
M-V type Object100002684.
M-V type PhysicalEntity100001930.