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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.

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  • CTS (rocket stage) (en)
  • CTS (tahapan roket) (in)
  • CTS (ロケットエンジン) (ja)
rdfs:comment
  • 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)
  • 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)
  • CTSはSSOのような(高度400km未満の)低軌道の用途においてCALTによって長征2号Cの性能を向上するために開発された上段ロケットである。 2段式の長征2号はペイロードを楕円軌道に投入してCTSは速度を補正して軌道を円軌道(SRM)にするために固体燃料ロケットに点火する。その間に衛星は運用に向けて準備する。 (ja)
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  • CTS (en)
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  • CTS:2 (en)
  • SD: 7 (en)
  • SMA:2 (en)
country
first
  • CTS: 2003-12-29 (en)
  • SD: 1997-09-01 (en)
  • SMA:2008-09-06 (en)
last
  • CTS: 2004-07-26 (en)
  • SD: 1999-06-12 (en)
  • SMA:2012-10-14 (en)
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  • 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)
  • 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)
  • CTSはSSOのような(高度400km未満の)低軌道の用途においてCALTによって長征2号Cの性能を向上するために開発された上段ロケットである。 2段式の長征2号はペイロードを楕円軌道に投入してCTSは速度を補正して軌道を円軌道(SRM)にするために固体燃料ロケットに点火する。その間に衛星は運用に向けて準備する。 (ja)
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launches
  • CTS:2 (en)
  • SD: 7 (en)
  • SMA:2 (en)
noburn
rockets
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