CZ-3B
Status | active |
---|---|
Country | China |
Manufacturer | China Academy of Launch Vehicle Technology |
Number of launches | 107 |
First launch | 1996-02-14 |
Last launch | 2025-04-10 |
Launches by year:
Latest launches:
Launch date | Launch site | Rocket / Variant | Payload | Status |
---|---|---|---|---|
2025-04-10 | Xichang | CZ-3B G2 | TJS 17 | success |
2025-03-26 | Xichang | CZ-3B G3 | Tianlian 2-04 | success |
2025-03-09 | Xichang | CZ-3B G2 | TJS 15 | success |
2025-02-22 | Xichang | CZ-3B G2 | Zhongxing-10R (ChinaSat 10R) | success |
2025-01-23 | Xichang | CZ-3B G2 | TJS 14 | success |
2025-01-06 | Xichang | CZ-3B G2 | Shijian 25 | success |
2024-12-20 | Xichang | CZ-3B G2 | TJS 12 | success |
2024-12-03 | Xichang | CZ-3B G2 | TJSW 13 | success |
2024-10-10 | Xichang | CZ-3B G3 | HGW-03 | success |
2024-09-19 | Xichang | CZ-3B G3 | Beidou-3 M27 / M28 | success |
+ 97 more... |
Variants:
(This section is under construction)CZ-3B
First launch | 1996-02-14 |
---|---|
Stages | 3 |
Boosters | 4 |
Mass | 425.8 t |
Height | 54.8 m |
Payload capacity:
LEO | 11200 kg to 200 km / 28.50 deg |
---|---|
GTO | 5100 kg |
Medium-lift orbital launch vehicle, developed by the China Academy of Launch Vehicle Technology (CALT). It is part of the Long March 3 series and is specifically designed for launching larger payloads into geostationary transfer orbit (GTO)
CZ-3B G2 (3B/E)
First launch | 2007-05-13 |
---|---|
Stages | 3 |
Boosters | 4 |
Mass | 458.9 t |
Height | 56.3 m |
Payload capacity:
GTO | 5500 kg |
---|
Developed from the CZ-3B with a lengthened first core stage and strap-on boosters, increasing the GTO capacity up to 5,500kg.
CZ-3B G3
First launch | 2011-09-18 |
---|---|
Stages | 3 |
Boosters | 4 |
CZ-3B G1
First launch | 2012-04-30 |
---|---|
Stages | 3 |
Boosters | 4 |
CZ-3B G3Z
First launch | 2013-12-01 |
---|---|
Stages | 4 |
Boosters | 4 |
Upper stage | Yuanzheng-1 |
CZ-3B G5
First launch | 2020-12-06 |
---|---|
Stages | 3 |
Boosters | 4 |
Mass | 456 t |
Height | 58 m |
Variant with a longer fairing.