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Wenchang LC101

Launch vehicle · China

Original archive entry. The text, images and links below are kept as they were written.

Launch complex for the CZ-5 launch vehicle.

Country
China
Launch Vehicles
Chang Zheng 5

Chronology

2 events

2016 November 3

12:43 GMT - . Launch Site: Wenchang. Launch Complex: Wenchang LC101. LV Family: CZ-NGLV. Launch Vehicle: Chang Zheng 5.
  • Shi Jian 17 - . Payload: SJ-17. Nation: China. Class: Communications. Type: Communications satellite. Spacecraft: DFH-4. USAF Sat Cat: 41838 . COSPAR: 2016-065A. Apogee: 35,804 km (22,247 mi). Perigee: 35,771 km (22,227 mi). Inclination: 0.80 deg.

    First launch from Wenchang Space Centre in Hainan. The CZ-5 configuration used four large liquid strapon boosters around a central 5 metre diameter core stage, with a second stage consisting of a stepped cylinder similar in configuration to the Delta 4/H-2A second stages. On this mission a Yuanzheng-2 third stage was also installed. The payload was Shi Jian 17, an experimental communications technology satellite with a secondary experiment to observe orbital debris. After launch at 1243 UTC the CZ-5 second stage achieved a 170 km parking orbit at 1257 UTC. At 1307 UTC the second stage made a six-minute-long second burn to 178 x 29127 km x 19.5 deg. The YZ-2 separated at 1313 UTC and shortly afterwards made a burn to 212 x 35802 km x 19.5 deg. YZ-2 then coasted to apogee and restarted at 1836 UTC to place itself in near geosynchronous orbit. The SJ-17 payload separated at about 1855 UTC into a 35886 x 38811 km x 0.8 deg orbit and drifted around the GEO arc. On Nov 12 it entered a 35771 x 35804 km geostationary orbit over 162.9E.

2017 July 2

11:22 GMT - . Launch Site: Wenchang. Launch Complex: Wenchang LC101. LV Family: CZ-NGLV. Launch Vehicle: Chang Zheng 5.
  • Shi Jian 18 - . Payload: SJ-18. Nation: China. COSPAR: 2017-F03. See SJ 18. ..