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CASC · Operational · cn · Launch Vehicle

Long March 3B

China's primary GTO workhorse; 5 launches in 2025.

Verified 2026-06-17 · First flight 1996-02-14

Operator page

Systems cutaway

Systems
Long March 3B — systems cutaway schematicPropulsion
YF-21C core + 4× YF-25 strap-ons (UDMH/N2O4); 5,922 kN liftoff thrust; YF-75D LOX/LH2 third stage.
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Structures
3.35 m core diameter; 54.8 m height; four liquid strap-on boosters.
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Long March 3B54.8 m
Propulsion

YF-21C core + 4× YF-25 strap-ons (UDMH/N2O4); 5,922 kN liftoff thrust; YF-75D LOX/LH2 third stage.

Structures

3.35 m core diameter; 54.8 m height; four liquid strap-on boosters.

Specs & Metrics

Payload to LEO ↑ better
11,500 kg
Maximum payload mass deliverable to low Earth orbit (~200–400 km circular), in the vehicle's stated reference configuration.
Payload to GTO ↑ better
5,500 kg
3B/E enhanced variant; standard 3B ~5,100 kg
Maximum payload mass deliverable to geostationary transfer orbit (~185 × 35,786 km), in the stated reference config.
Liftoff Thrust ↑ better
5922 kN
core 2,962 kN + 4× booster 740 kN each
Total first-stage thrust at liftoff (sea-level), in kilonewtons, summing all active engines and solid strap-ons.
Vehicle Height ↓ better
54.8 m
Full stack height at liftoff, in metres, including fairing or spacecraft.
Mission Success Rate ↑ better
95.7%
110 successes, 5 failures per RocketLaunch.org
Percentage of launch attempts rated as full mission successes over the vehicle's complete flight history.
Launches in 2025 ↑ better
5
Total number of launch attempts conducted in calendar year 2025 (Jan 1 – Dec 31 UTC).

Subsystems

propulsion

YF-21C core + 4× YF-25 strap-ons (UDMH/N2O4); 5,922 kN liftoff thrust; YF-75D LOX/LH2 third stage.

structures

3.35 m core diameter; 54.8 m height; four liquid strap-on boosters.