Notice: file_put_contents(): Write of 32232 bytes failed with errno=28 No space left on device in /opt/frankenphp/design.onmedianet.com/app/src/Arsae/CacheManager.php on line 36

Warning: http_response_code(): Cannot set response code - headers already sent (output started at /opt/frankenphp/design.onmedianet.com/app/src/Arsae/CacheManager.php:36) in /opt/frankenphp/design.onmedianet.com/app/src/Models/Response.php on line 17

Warning: Cannot modify header information - headers already sent by (output started at /opt/frankenphp/design.onmedianet.com/app/src/Arsae/CacheManager.php:36) in /opt/frankenphp/design.onmedianet.com/app/src/Models/Response.php on line 20
CZ-6 (Chang Zheng-6)
Please make a donation to support Gunter's Space Page.
Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.

CZ-6 (Chang Zheng-6)

CZ-6 (Flight 1) [Xinhua]

CZ-6 (Qilu 1, 4) [Xinhua]

CZ-6A (Tiankun 2, Pujiang 2)
[Chinaspaceflight]

CZ-6C (Haiwangxing 01)
[Chinaspaceflight]

The CZ-6 (Chang Zheng-6), also known as LM-6 (Long March-6), is a small liquid fueled launch vehicle in the CZ-5, -6 and -7 family.

The launch vehicle was developed by China Aerospace Science and Technology Corporation and the China Academy of Launch Vehicle Technology.

CZ-6 features a 3.35 m diameter first stage fueled with LOX and Kerosene and powered by one YF-100 engine. Originally the vehicle was to be based on the 2.25 m small strap on of the CZ-5 family, but was changed to the 3.35 m diameter of the bigger booster and the CZ-7 family, although shorter and using only one instead of two engines.

The second stage has the smaller 2.25 m diameter and uses the same fuels with one YF-115 engine.

A restartable third stage reportedly uses the storable combination of Kerosene and Hydrogen peroxide. With four YF-85 engines it provides final orbit trim and can manoeuvre to different orbits to deploy multiple satellites.

CZ-6 can deliver 1500 kg into a low earth orbit or 1080 kg into a 700 km sun synchronous orbit.

Taiyuan is used as a launch site for the maiden launch in 2015, although later the new Wenchang cosmodrome will also be used.

An improved CZ-6A (Chang Zheng-6A) is planned to be introduced during the 13th Five Year Plan (2016-2020). It features 4 strap-on boosters of 1 m diameter, a lengthened stage one, a new stage two with the same diameter as stage one. It is planned to put up to 4000 kg into a sun-synchronous orbit.

Version Strap-On Stage 1 Stage 2 Stage 3
CZ-6 - K-3-0 (?) / YF-100 K-2-2 / YF-115 ? / 4 × YF-85
CZ-6A 4 × ? stretched K-3-0 (?) / 2 × YF-100 ? ?
CZ-6C - stretched K-3-0 (?) / 2 × YF-100K 2.9 m stage / YF-115 -
Performance (kg) LEO LPEO SSO GTO GEO MolO IP
CZ-6 1500 1080 - - - -
CZ-6A 4500 - - - -
CZ-6C 2500 - - - -
No:       Type:             Serial    Date            LS            Payload

 1    1   CZ-6              6-Y1      19.09.2015      TY LC-16      XY 2 / DCBB / ZDPS 2A / ZDPS 2B / XW 2A / XW 2B / XW 2C / XW 2D / XW 2E / XW 2F / LilacSat 2 / Naxing 2 / ZJ 1 /
                                                                    KJSY 1 / Tiantuo 3 / NUDT-PhoneSat / XC 1 / XC 2 / XC 3 / XC 4
 2    2   CZ-6              6-Y2      21.11.2017      TY LC-16      Jilin-1 Shipin-04 / Jilin-1 Shipin-05 / Jilin-1 Shipin-06
 3    3   CZ-6              6-Y4      13.11.2019      TY LC-16      Zhongzi 1-01, ..., 1-05
 4    4   CZ-6              6-Y3      06.11.2020      TY LC-16      ÑuSat 9, ..., 18 / Beihangkongshi 1 / Tianyan 05 / BY 3
 5    5   CZ-6              6-Y5      27.04.2021      TY LC-16      Qilu 1 / Qilu 4 / Foshan 1 / Hangsheng 1 / Tianqi 9 / NEO 1 / Taijing-2 01 / Jinzijing 1-01 / Jinzijing 1-02
 6    6   CZ-6              6-Y6      09.07.2021      TY LC-16      Zhongzi 2-01, ..., 2-05
 7    7   CZ-6              6-Y7      04.08.2021      TY LC-16      KL-Beta A / KL-Beta B
 8    8   CZ-6              6-Y8      05.11.2021      TY LC-16      Guangmu 1 (SDGSAT 1)
 9    1   CZ-6A             6A-Y1     29.03.2022      TY LC-9A      Pujiang 2 / Tiankun 2
10    9   CZ-6              6-Y10     10.08.2022      TY LC-16      Jilin-1 Gaofen-03D-09, 03D-35, ..., 03D-43 / Jilin-1 Hongwai-A01, ..., A06
11   10   CZ-6              6-Y9      26.09.2022      TY LC-16      Shiyan 16A / Shiyan 16B / SY 17
12    2   CZ-6A             6A-Y2     11.11.2022      TY LC-9A      Yunhai-3 01
13   11   CZ-6              6-Y12     20.06.2023      TY LC-16      Shiyan 25
14    3   CZ-6A             6A-Y5     10.09.2023      TY LC-9A      Yaogan 40-01A / Yaogan 40-01B / Yaogan 40-01C
15    4   CZ-6A             6A-Y4     31.10.2023      TY LC-9A      Tianhui 5A / Tianhui 5B
16    5   CZ-6A             6A-Y.     26.03.2024      TY LC-9A      Yunhai-3 02
17    1   CZ-6C             6C-Y1     07.05.2024      TY LC-9A      Haiwangxing 01 / Zhixing 1C / Kuanfu Guangxue / Gaofen Shipin
18    6   CZ-6A             6A-Y7     04.07.2024      TY LC-9A      Tianhui 5C / Tianhui 5D
19    7   CZ-6A             6A-Y21    06.08.2024      TY LC-9A      Qianfan Jigui G01-01, ..., G01-18
20   12   CZ-6              6-Y.      05.09.2024      TY LC-16      GeeSAT 3-1, ..., 3-10
21    8   CZ-6A             6A-Y20    15.10.2024      TY LC-9A      Qianfan Jigui G02-01, ..., G02-18Qianfan Jigui G01-01, ..., G01-18
22   13   CZ-6              6-Y13     22.10.2024      TY LC-16      Tianping 3A-01 / Tianping 3B-01 / Tianping 3B-02
23    9   CZ-6A             6A-Y.     05.12.2024      TY LC-9A      Qianfan Jigui G03-01, ..., G03-18
24   10   CZ-6A             6A-Y.     23.01.2025      TY LC-9A      Qianfan Jigui G06-01, ..., G06-18
25   14   CZ-6              6-Y.      03.04.2025      TY LC-16      Tianping 3A-02
26   11   CZ-6A             6A-Y11    18.04.2025      TY LC-9A      Shiyan 27A / Shiyan 27B / Shiyan 27C / Shiyan 27D / Shiyan 27E / Shiyan 27F
27   12   CZ-6A             6A-Y.     11.05.2025      TY LC-9A      Yaogan 40-02A / Yaogan 40-02B / Yaogan 40-02C
28   13   CZ-6A             6A-Y8     05.06.2025      TY LC-9A      HWD L04-01, ..., L04-05
29   14   CZ-6A             6A-Y14    27.07.2025      TY LC-9A      HWD L05-01, ..., L05-05
30   15   CZ-6A             6A-Y      17.08.2025      TY LC-9A      HWD L09-01, ..., L09-05
31   16   CZ-6A             6A-Y.     06.09.2025      TY LC-9A      Yaogan 40-03A / Yaogan 40-03B / Yaogan 40-03C
32   17   CZ-6A             6A-Y18    27.09.2025      TY LC-9A      HWD L11-01, ..., L11-05


Planned:


Launch sites:

TY  =    Taiyuan Satellite Launch Center (TSLC), Wuzhai, Shanxi, China   China
We  =    Wenchang Space Launch Center (WSLC), Hainan, China   China


F       Failure
P       Partial Failure

Cite this page: