The CTS is an upper stage developed by the China Academy of Launch Vehicle Technology (CALT) to improve the performance of the Long March 2C to high (>400 km of altitude) LEO missions like SSO. The two stage LM-2 delivers the payload and stage to an elliptical orbit with the desired apogee and the CTS points the stack in the direction of the correct vector and activates the solid rocket motor (SRM) main engine to circularize it. It then dispenses the spacecraft and does a passivisation procedure.

Property Value
dbo:abstract
  • CTS adalah tahap atas yang dikembangkan oleh CALT untuk meningkatkan kinerja Long March 2C ke tinggi (> 400 km dari ketinggian) misi LEO seperti SSO. (in)
  • The CTS is an upper stage developed by the China Academy of Launch Vehicle Technology (CALT) to improve the performance of the Long March 2C to high (>400 km of altitude) LEO missions like SSO. The two stage LM-2 delivers the payload and stage to an elliptical orbit with the desired apogee and the CTS points the stack in the direction of the correct vector and activates the solid rocket motor (SRM) main engine to circularize it. It then dispenses the spacecraft and does a passivisation procedure. (en)
dbo:wikiPageID
  • 47338355 (xsd:integer)
dbo:wikiPageLength
  • 10035 (xsd:integer)
dbo:wikiPageRevisionID
  • 960761126 (xsd:integer)
dbp:country
dbp:derivatives
dbp:derivedFrom
dbp:fail
  • 0 (xsd:integer)
dbp:first
  • CTS: 2003-12-29 (en)
  • SD: 1997-09-01 (en)
  • SMA:2008-09-06 (en)
dbp:last
  • CTS: 2004-07-26 (en)
  • SD: 1999-06-12 (en)
  • SMA:2012-10-14 (en)
dbp:launches
  • CTS:2 (en)
  • SD: 7 (en)
  • SMA:2 (en)
dbp:manufacturer
dbp:name
  • CTS (en)
dbp:noburn
  • 0 (xsd:integer)
dbp:rockets
  • --03-02
dbp:success
  • CTS:2 (en)
  • SD: 7 (en)
  • SMA:2 (en)
dbp:wikiPageUsesTemplate
dct:subject
rdfs:comment
  • CTS adalah tahap atas yang dikembangkan oleh CALT untuk meningkatkan kinerja Long March 2C ke tinggi (> 400 km dari ketinggian) misi LEO seperti SSO. (in)
  • The CTS is an upper stage developed by the China Academy of Launch Vehicle Technology (CALT) to improve the performance of the Long March 2C to high (>400 km of altitude) LEO missions like SSO. The two stage LM-2 delivers the payload and stage to an elliptical orbit with the desired apogee and the CTS points the stack in the direction of the correct vector and activates the solid rocket motor (SRM) main engine to circularize it. It then dispenses the spacecraft and does a passivisation procedure. (en)
rdfs:label
  • CTS (rocket stage) (en)
  • CTS (tahapan roket) (in)
owl:sameAs
prov:wasDerivedFrom
foaf:isPrimaryTopicOf
is dbo:wikiPageDisambiguates of
is dbo:wikiPageRedirects of
is dbp:derivatives of
is dbp:derivedFrom of
is dbp:usedIn of
is foaf:primaryTopic of