Yuanzheng Explained

Yuanzheng
Manufacturer:CALT
Country:China
Rockets:Long March rocket family
(2C 2D 3B 3C 5 7)
Comparable:Fregat
Status:Active
Launches:29
Success:28
Fail:1
Noburn:0
First:30 March 2015
BeiDou I1-S
Last:21 March 2024
Yunhai-2 Group 02
Only:
Yuanzheng
Engines:1 × YF-50D
Si:315.5 seconds
Fuel: / UDMH

Yuanzheng is a restartable upper stage developed by the China Academy of Launch Vehicle Technology (CALT) for the Long March rocket family.

The Yuanzheng stage enables the Chinese launch vehicles to deploy payloads directly to high-energy orbits such as medium Earth orbit (MEO) and geosynchronous orbit (GSO). Since the Long March third stage cannot restart, it cannot circularize a GSO or GEO orbit from a geosyncronous transfer orbit (GTO). With its restart capability, Yuanzheng has enabled the deployment of satellite pairs for the BeiDou Navigation Satellite System in MEO and communications satellites in GSO. This eliminates the need for the spacecraft to include a liquid apogee engine or an apogee kick motor.

Yuanzheng has a thrust of with a specific impulse of 315.5 seconds. It uses the storable hypergolic propellants unsymmetrical dimethylhydrazine (UDMH) and dinitrogen tetroxide, and can perform at least two burns within its rated life of 6.5 hours, sufficient to reach the transfer orbit apogee, and perform the circularization burn from there.

Operational variants are designated YZ-1 for Long March 3B and 3C, YZ-1A for Long March 7, YZ-1S for Long March 2C, YZ-2 for Long March 5, and YZ-3 for Long March 2D.

History

Yuanzheng was presented in a 2013 paper and performed its first mission on 30 May 2015. The debut flight of the Long March 7 in 2016 included an improved version called Yuanzheng-1A that can flexibly deploy multiple payloads into various target orbits. Further variants were later deployed for Long March 5 (YZ-2) in 2016, Long March 2C (YZ-1S) and Long March 2D (YZ-3) in 2018.

FlightNo.Date (UTC)Carrier RocketStage ModelSerial NumberLaunch siteMissionResult
1 2015-03-30
13:52
YZ-1 Y1
2 2015-07-25
12:29
YZ-1 Y2
3 2016-02-01
07:29
YZ-1 Y3
4 2016-06-25
12:00
YZ-1A Y1 Inaugural Mission
5 2016-11-3
12:43
YZ-2 Y1 Inaugural Mission
6 2017-11-5
11:45
YZ-1 Y4
7 2018-01-11
23:18
YZ-1 Y5
8 2018-02-12
05:03
YZ-1 Y6
9 2018-03-29
17:56
YZ-1 Y7
10 2018-07-29
01:48
YZ-1 Y8
11 2018-08-24
23:52
YZ-1 Y9
12 2018-09-19
14:07
YZ-1 Y10
13 2018-10-09
02:43
YZ-1S Y1 Yaogan 32A, 32B
14 2018-10-15
04:23
YZ-1 Y11
15 2018-11-18
18:00
YZ-1 Y12
16 2018-12-29
08:00
YZ-3 Y1 Yunhai-2 01, 02, 03, 04, 05, 06
Hongyan-1
17 2019-09-22
21:10
Long March 3B/E YZ-1 Y13 Xichang
18 2019-11-23
00:55
Long March 3B/E YZ-1 Y14 Xichang
19 2019-12-16
07:22
Long March 3B/E YZ-1 Y15 Xichang
20 2021-08-24
11:15
YZ-1S Y2 JiuquanRSW-01
RSW-02
unknown payload
21 2021-11-03
07:43
YZ-1S Y4 JiuquanYaogan 32-02A, 32-02B
22 2022-05-20
10:30
YZ-1S Y5 JiuquanLEO Test Sat 1/2
Digui Tongxin Weixing
23 2023-07-09
11:00
YZ-1S Y3 JiuquanHulianwang Jishu Shiyan 1A
Hulianwang Jishu Shiyan 1B
24 2023-11-16
03:55
YZ-1S Y9 Jiuquan
25 2023-11-23
10:00
YZ-3 Y2 XichangHulianwang Jishu Shiyan 2A
Hulianwang Jishu Shiyan 2B
Hulianwang Jishu Shiyan 2C
26 2023-12-26
03:26
Long March 3B/E YZ-1 Y16 Xichang
27 2023-12-30
00:13
YZ-1S Y17 JiuquanHulianwang Jishu Shiyan 4A
Hulianwang Jishu Shiyan 4B
Hulianwang Jishu Shiyan 4C
28 2024-03-13
12:51
YZ-1S Y18 XichangDRO-A/B
29 2024-03-21
05:27
YZ-3 Y3 JiuquanYunhai-2 Group 02

Versions

Currently, there is known to be five versions: