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- Q53702 subject Q7008582.
- Q53702 abstract "Long March 2C (LM-2C), or Chang Zheng 2C (CZ-2C) as in Chinese pinyin is a member of the Long March 2 rocket family, an expendable launch system operated by the People's Republic of China. This vehicle was developed by the China Academy of Launch Vehicle Technology, and the first launch occurred on September 9, 1982. It is a two-stage launch vehicle with storable propellants, consisting of Nitrogen Tetroxide and Unsymmetrical Dimethyl Hydrazine. The rocket was derived from the Long March 2A launch vehicle.Several variants of this launch vehicle have been built, all using an optional third solid motor stage: 2C/SD — Commercial satellite launcher with a multi-satellite smart dispenser allowing delivery of two satellites simultaneously 2C/SM — Version for delivery of small satellites to high orbits 2C/SMA — Improved version of the 2C/SM↑ 1.0 1.1 ↑".
- Q53702 countryOrigin Q148.
- Q53702 diameter "3.35".
- Q53702 failedLaunches "1".
- Q53702 height "42.0".
- Q53702 launchSite Q1194479.
- Q53702 launchSite Q692677.
- Q53702 launchSite Q734306.
- Q53702 maidenFlight "1982-09-09".
- Q53702 manufacturer Q5099556.
- Q53702 mass "2.33E8".
- Q53702 rocketFunction Q697175.
- Q53702 rocketStages "2".
- Q53702 status "Active".
- Q53702 successfulLaunches "40".
- Q53702 thumbnail CZ-2C.svg?width=300.
- Q53702 totalLaunches "41".
- Q53702 wikiPageExternalLink index.html.
- Q53702 wikiPageWikiLink Q1138649.
- Q53702 wikiPageWikiLink Q1194479.
- Q53702 wikiPageWikiLink Q148.
- Q53702 wikiPageWikiLink Q15078724.
- Q53702 wikiPageWikiLink Q161296.
- Q53702 wikiPageWikiLink Q174241.
- Q53702 wikiPageWikiLink Q174706.
- Q53702 wikiPageWikiLink Q20944070.
- Q53702 wikiPageWikiLink Q218056.
- Q53702 wikiPageWikiLink Q2672736.
- Q53702 wikiPageWikiLink Q2981398.
- Q53702 wikiPageWikiLink Q3115617.
- Q53702 wikiPageWikiLink Q382984.
- Q53702 wikiPageWikiLink Q42222.
- Q53702 wikiPageWikiLink Q49939.
- Q53702 wikiPageWikiLink Q5099556.
- Q53702 wikiPageWikiLink Q53665.
- Q53702 wikiPageWikiLink Q53700.
- Q53702 wikiPageWikiLink Q589786.
- Q53702 wikiPageWikiLink Q6203431.
- Q53702 wikiPageWikiLink Q663611.
- Q53702 wikiPageWikiLink Q692677.
- Q53702 wikiPageWikiLink Q697175.
- Q53702 wikiPageWikiLink Q7008582.
- Q53702 wikiPageWikiLink Q734306.
- Q53702 wikiPageWikiLink Q7496500.
- Q53702 wikiPageWikiLink Q909335.
- Q53702 countryOrigin Q148.
- Q53702 fail "1".
- Q53702 first "1982-09-09".
- Q53702 function Q697175.
- Q53702 launches "41".
- Q53702 manufacturer Q5099556.
- Q53702 sites Q1194479.
- Q53702 sites Q6203431.
- Q53702 sites Q692677.
- Q53702 sites Q734306.
- Q53702 stages "2".
- Q53702 status "Active".
- Q53702 success "40".
- Q53702 type MeanOfTransportation.
- Q53702 type Rocket.
- Q53702 type DesignedArtifact.
- Q53702 type Thing.
- Q53702 type Q41291.
- Q53702 comment "Long March 2C (LM-2C), or Chang Zheng 2C (CZ-2C) as in Chinese pinyin is a member of the Long March 2 rocket family, an expendable launch system operated by the People's Republic of China. This vehicle was developed by the China Academy of Launch Vehicle Technology, and the first launch occurred on September 9, 1982. It is a two-stage launch vehicle with storable propellants, consisting of Nitrogen Tetroxide and Unsymmetrical Dimethyl Hydrazine.".
- Q53702 label "Long March 2C".
- Q53702 depiction CZ-2C.svg.