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PLA2AC
Di Er Paobing Budui, Zhongguo Renmin Jeifangjun
Location: Beijing.
Country:
China.
1996 March 7 - .
16:00 GMT - .
Launch Site:
Leping.
Launch Vehicle:
DF-15.
- Near Taiwan - .
Nation: China.
Agency: PLA2AC.
Apogee: 100 km (60 mi).
1996 March 7 - .
17:00 GMT - .
Launch Site:
Leping.
Launch Vehicle:
DF-15.
- Near Taiwan - .
Nation: China.
Agency: PLA2AC.
Apogee: 100 km (60 mi).
1996 March 7 - .
18:00 GMT - .
Launch Site:
Leping.
Launch Vehicle:
DF-15.
- Near Taiwan - .
Nation: China.
Agency: PLA2AC.
Apogee: 100 km (60 mi).
1996 March 13 - .
Launch Site:
Leping.
Launch Vehicle:
DF-15.
- Near Taiwan - .
Nation: China.
Agency: PLA2AC.
Apogee: 100 km (60 mi).
2005 June 9 - .
Launch Site:
Taiyuan.
LV Family:
DF-31.
Launch Vehicle:
KT-1.
FAILURE: Reported orbital launch failure.
- MS-1? - .
Nation: China.
Agency: PLA2AC.
Apogee: 300 km (180 mi).
2012 March 17 - .
Launch Site:
Jiuquan.
LV Family:
DF-21.
Launch Vehicle:
Kuaizhou.
- Test payload? - .
Nation: China.
Agency: PLA2AC.
Apogee: 200 km (120 mi). Maybe orbital attempt.
2012 November 30 - .
Launch Site:
Taiyuan.
Launch Vehicle:
DF-31.
- Nation: China.
Agency: PLA2AC.
Apogee: 1,000 km (600 mi).
2013 January 27 - .
12:10 GMT - .
Launch Site:
Jiuquan.
LV Family:
DF-11.
Launch Vehicle:
B-611.
- Target RV - .
Nation: China.
Agency: PLA2AC.
Type: ABM Target. Apogee: 100 km (60 mi). ABM Target.
2013 July 24 - .
Launch Site:
Taiyuan.
Launch Vehicle:
DF-31.
- Nation: China.
Agency: PLA2AC.
Apogee: 1,000 km (600 mi).
2014 January 9 - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- Hypersonic RV - .
Nation: China.
Agency: PLA2AC.
Apogee: 40 km (24 mi).
2014 July 23 - .
Launch Site:
Urumqi.
Launch Vehicle:
DF-21.
- Nation: China.
Agency: PLA2AC.
Apogee: 250 km (150 mi).
2014 July 23 - .
Launch Site:
Jiuquan.
LV Family:
DF-11.
Launch Vehicle:
B-611.
2014 August 7 - .
Launch Site:
Taiyuan.
LV Family:
CZ.
Launch Vehicle:
Chang Zheng 2C.
- Hypersonic RV - .
Nation: China.
Agency: PLA2AC.
Apogee: 40 km (24 mi). Claimed to be a test of a hypersonic glide reentry vehicle. Based on images from the impact
site of one of the stages, the launch appeared to have used a large liquid fuelled booster, possibly a modified CZ-2C..
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