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- Yuanzheng-1 abstract "The Yuanzheng-1 (AKA YZ-1) is an upper stage developed by CALT to enable the Long March 3B and Long March 3C to deploy directly to high energy orbits like MEO and GSO. Since the third stage of these rocket can not restart, it can not circularize orbit from a GTO transfer. Not only the restart capabilities are required, but the upper stage had the remain operational during the time to reach the orbit apogee to execute the circularization burn. For a standard GTO transfer, this is of around 6 hours. The YZ-1 was developed to meet these requirements and enabled the deployment of satellite pairs for BeiDou directly to their orbits or communications satellite directly to GSO. This way, the spacecrafts do not need an LAE or APK.It has a thrust of 6.5 kN (1,500 lbf) with an isp of 315.5 seconds. It uses the storable propellant N2O4/UDMH can perform at least two burn within its rated life of 6.5 hours.".
- Yuanzheng-1 wikiPageID "47350094".
- Yuanzheng-1 wikiPageLength "5242".
- Yuanzheng-1 wikiPageOutDegree "40".
- Yuanzheng-1 wikiPageRevisionID "702884082".
- Yuanzheng-1 wikiPageWikiLink Apogee_kick_motor.
- Yuanzheng-1 wikiPageWikiLink BeiDou_Navigation_Satellite_System.
- Yuanzheng-1 wikiPageWikiLink Category:Rocket_stages.
- Yuanzheng-1 wikiPageWikiLink China.
- Yuanzheng-1 wikiPageWikiLink China_Academy_of_Launch_Vehicle_Technology.
- Yuanzheng-1 wikiPageWikiLink Dinitrogen_tetroxide.
- Yuanzheng-1 wikiPageWikiLink Fregat.
- Yuanzheng-1 wikiPageWikiLink Geostationary_orbit.
- Yuanzheng-1 wikiPageWikiLink Geostationary_transfer_orbit.
- Yuanzheng-1 wikiPageWikiLink Liquid_Apogee_Engine.
- Yuanzheng-1 wikiPageWikiLink Long_March_3.
- Yuanzheng-1 wikiPageWikiLink Long_March_3B.
- Yuanzheng-1 wikiPageWikiLink Long_March_3C.
- Yuanzheng-1 wikiPageWikiLink Long_March_5.
- Yuanzheng-1 wikiPageWikiLink Medium_Earth_orbit.
- Yuanzheng-1 wikiPageWikiLink Multistage_rocket.
- Yuanzheng-1 wikiPageWikiLink Specific_impulse.
- Yuanzheng-1 wikiPageWikiLink Unsymmetrical_dimethylhydrazine.
- Yuanzheng-1 wikiPageWikiLink Xichang_Satellite_Launch_Center.
- Yuanzheng-1 wikiPageWikiLinkText "YZ-1".
- Yuanzheng-1 wikiPageWikiLinkText "Yuanzheng-1".
- Yuanzheng-1 wikiPageWikiLinkText "Yuanzheng-2".
- Yuanzheng-1 comparable Fregat.
- Yuanzheng-1 country China.
- Yuanzheng-1 engines "1".
- Yuanzheng-1 fail "0".
- Yuanzheng-1 first "2015-03-30".
- Yuanzheng-1 first "BDS I1-S Mission".
- Yuanzheng-1 fuel Dinitrogen_tetroxide.
- Yuanzheng-1 fuel Unsymmetrical_dimethylhydrazine.
- Yuanzheng-1 launches "3".
- Yuanzheng-1 manufacturer China_Academy_of_Launch_Vehicle_Technology.
- Yuanzheng-1 name "Yuanzheng-1".
- Yuanzheng-1 noburn "0".
- Yuanzheng-1 rockets "--03-03".
- Yuanzheng-1 si "315.5".
- Yuanzheng-1 status "Active".
- Yuanzheng-1 success "3".
- Yuanzheng-1 wikiPageUsesTemplate Template:Convert.
- Yuanzheng-1 wikiPageUsesTemplate Template:Infobox_rocket_stage.
- Yuanzheng-1 wikiPageUsesTemplate Template:Reflist.
- Yuanzheng-1 wikiPageUsesTemplate Template:Upper_stages.
- Yuanzheng-1 subject Category:Rocket_stages.
- Yuanzheng-1 hypernym Stage.
- Yuanzheng-1 type Person.
- Yuanzheng-1 type Rocket.
- Yuanzheng-1 comment "The Yuanzheng-1 (AKA YZ-1) is an upper stage developed by CALT to enable the Long March 3B and Long March 3C to deploy directly to high energy orbits like MEO and GSO. Since the third stage of these rocket can not restart, it can not circularize orbit from a GTO transfer. Not only the restart capabilities are required, but the upper stage had the remain operational during the time to reach the orbit apogee to execute the circularization burn.".
- Yuanzheng-1 label "Yuanzheng-1".
- Yuanzheng-1 sameAs Q20871633.
- Yuanzheng-1 sameAs Yuanzheng-1.
- Yuanzheng-1 sameAs Q20871633.
- Yuanzheng-1 sameAs 远征一号.
- Yuanzheng-1 wasDerivedFrom Yuanzheng-1?oldid=702884082.
- Yuanzheng-1 isPrimaryTopicOf Yuanzheng-1.