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Launch Vehicle Comparison

Comprehensive database of active, in-development, and retired orbital launch vehicles worldwide with real specifications, reliability data, and cost analysis

24
Vehicles Tracked
19
Operational
4
In Development
1,052
Total Launches
Status:
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Showing 24 of 24 launch vehicles

Starship / Super Heavy

SpaceX|US
In Development
Payload LEO150,000 kg
Payload GTO21,000 kg
Height121 m
Cost$10M
Reliability42.9% (3/7)
Reusable2-StageCH4

The largest and most powerful rocket ever flown, designed for full and rapid reusability. Intended to enable Mars colonization, point-to-point Earth transport, and dramatically reduce cost per kg to orbit. Tower catch of the Super Heavy booster demonstrated in 2024.

Falcon Heavy

SpaceX|US
Operational
Payload LEO63,800 kg
Payload GTO26,700 kg
Height70 m
Cost$97M
Reliability100.0% (12/12)
Reusable2-StageRP-1

The most powerful operational rocket by payload capacity to LEO. Uses three Falcon 9 first-stage cores strapped together. Side boosters are routinely recovered; center core recovery has been demonstrated.

New Glenn

Blue Origin|US
Operational
Payload LEO45,000 kg
Payload GTO13,000 kg
Height98 m
Cost$68M
Reliability50.0% (1/2)
Reusable2-StageCH4

Blue Origin's orbital heavy-lift launch vehicle with a reusable first stage. Features the largest payload fairing in production at 7 meters diameter. Named after astronaut John Glenn. Targets commercial, civil, and national security launches.

Vulcan Centaur

ULA|US
Operational
Payload LEO27,200 kg
Payload GTO12,350 kg
Height61.6 m
Cost$110M
Reliability100.0% (3/3)
2-StageCH4

ULA's next-generation launch vehicle replacing both Atlas V and Delta IV Heavy. Uses Blue Origin BE-4 methalox engines on the first stage and the proven Centaur V upper stage with RL-10C engines. Designed for national security missions.

Long March 5

CALT / CASC|CN
Operational
Payload LEO25,000 kg
Payload GTO14,000 kg
Height56.97 m
Cost$100M
Reliability92.3% (12/13)
2-StageLH2

China's most powerful operational rocket, used for the Tianhe space station modules, Chang'e lunar missions, and Tianwen Mars probe. The Long March 5B variant is used for LEO heavy-lift.

Angara A5

Khrunichev|RU
Operational
Payload LEO24,500 kg
Payload GTO5,400 kg
Height64 m
Cost$100M
Reliability100.0% (4/4)
3-StageRP-1

Russia's new modular heavy-lift vehicle intended to replace the Proton-M. Built from Universal Rocket Modules (URMs). Unlike Proton, uses environmentally cleaner RP-1/LOX propellant. Launching from Vostochny Cosmodrome.

Proton-M

Khrunichev|RU
Operational
Payload LEO23,700 kg
Payload GTO6,920 kg
Height58.2 m
Cost$65M
Reliability90.4% (103/114)
4-StageUDMH

Russia's heavy-lift workhorse used primarily for GTO communications satellites and interplanetary missions. Uses hypergolic propellants throughout. Being phased out in favor of the Angara A5.

Falcon 9 Block 5

SpaceX|US
Operational
Payload LEO22,800 kg
Payload GTO8,300 kg
Height70 m
Cost$67M
Reliability99.5% (380/382)
Reusable2-StageRP-1

The workhorse of the global launch industry. First orbital-class rocket to achieve propulsive landing and routine reuse of the first stage. Dominates the global commercial launch market with the highest cadence of any active vehicle.

Ariane 6

ArianeGroup|EU
Operational
Payload LEO21,650 kg
Payload GTO11,500 kg
Height56 m
Cost$77M
Reliability50.0% (1/2)
2-StageLH2

Europe's newest heavy-lift launcher replacing Ariane 5. Available in A62 (2 SRBs) and A64 (4 SRBs) configurations. The Vinci upper stage engine features a restart capability for complex mission profiles.

Terran R

Relativity Space|US
In Development
Payload LEO20,000 kg
Payload GTO5,000 kg
Height66 m
CostTBD
Reusable2-StageCH4

A medium-to-heavy lift reusable launch vehicle incorporating 3D-printed manufacturing. Following the retirement of Terran 1 after its test flight, Relativity shifted focus entirely to Terran R for the medium-lift reusable market.

Atlas V

ULA|US
Retired
Payload LEO18,850 kg
Payload GTO8,900 kg
Height58.3 m
Cost$110M
Reliability99.0% (100/101)
2-StageRP-1

One of the most reliable launch vehicles ever built, with a near-perfect flight record over two decades. Used Russian RD-180 engines. Retired in 2024 after final mission, replaced by Vulcan Centaur.

H3

JAXA / MHI|JP
Operational
Payload LEO16,500 kg
Payload GTO6,500 kg
Height63 m
Cost$51M
Reliability75.0% (3/4)
2-StageLH2

Japan's next-generation flagship launch vehicle replacing the H-IIA. Features the expander-bleed cycle LE-9 engine, designed for improved reliability and reduced cost. Achieved first successful orbital flight in February 2024.

Neutron

Rocket Lab|US
In Development
Payload LEO13,000 kg
Payload GTO1,500 kg
Height43 m
Cost$50M
Reusable2-StageCH4

Rocket Lab's medium-lift reusable launch vehicle, targeting the mega-constellation deployment market. Features a unique "Hungry Hippo" fairing design integrated into the first stage, Archimedes methalox engines, and propulsive landing capability.

Long March 3B/E

CALT / CASC|CN
Operational
Payload LEO11,500 kg
Payload GTO5,500 kg
Height56.33 m
Cost$70M
Reliability95.7% (90/94)
3-StageUDMH/N2O4

China's primary GTO launch vehicle, used extensively for BeiDou navigation satellite deployment. Features four strap-on liquid boosters and a cryogenic third stage.

LVM3 (GSLV Mk III)

ISRO|IN
Operational
Payload LEO10,000 kg
Payload GTO4,000 kg
Height43.4 m
Cost$47M
Reliability100.0% (8/8)
3-StageHTPB

India's heaviest launch vehicle, used for Chandrayaan-3 lunar mission and OneWeb constellation deployment. Features indigenous CE-20 cryogenic upper stage engine. Also designated for the Gaganyaan crewed program.

Soyuz-2.1b

RKTs Progress|RU
Operational
Payload LEO8,200 kg
Payload GTO3,250 kg
Height46.3 m
Cost$48M
Reliability97.1% (66/68)
3-StageRP-1

The modern variant of the legendary R-7 derived Soyuz family, the most launched rocket design in history. Used for ISS crew transport (with Soyuz-2.1a for crewed flights), Glonass navigation, and commercial payloads.

Long March 6A

SAST / CASC|CN
Operational
Payload LEO7,000 kg
Payload GTO--
Height50 m
Cost$35M
Reliability100.0% (3/3)
2-StageRP-1

China's newest medium-lift hybrid vehicle combining liquid core stage with solid strap-on boosters. Designed for SSO constellation deployment with high launch cadence.

PSLV

ISRO|IN
Operational
Payload LEO3,800 kg
Payload GTO1,425 kg
Height44 m
Cost$21M
Reliability95.2% (59/62)
4-StageHTPB

India's highly reliable workhorse launcher with over 60 missions. Known for cost-effective rideshare and dedicated small satellite missions. Holds the record for deploying 104 satellites in a single mission (PSLV-C37).

Long March 2D

SAST / CASC|CN
Operational
Payload LEO3,500 kg
Payload GTO--
Height41.06 m
Cost$30M
Reliability98.9% (91/92)
2-StageUDMH

China's highly reliable medium-lift workhorse, primarily used for Earth observation and SSO missions. One of the most frequently launched Chinese vehicles with an excellent reliability record.

Vega-C

Avio|EU
Operational
Payload LEO2,300 kg
Payload GTO--
Height34.8 m
Cost$37M
Reliability66.7% (2/3)
4-StageHTPB

ESA's upgraded small-to-medium launch vehicle with improved performance over the original Vega. Uses the P120C solid motor shared with Ariane 6 as its first stage. Returned to flight in late 2024 after a Zefiro-40 nozzle failure.

Epsilon S

IHI Aerospace / JAXA|JP
In Development
Payload LEO1,500 kg
Payload GTO--
Height27.5 m
Cost$30M
3-StageSolid

Japan's upgraded solid-fuel small satellite launcher, enhanced from the Epsilon series. Shares the SRB-3 booster with H3. Development delayed by a third-stage static fire test failure in 2023.

Firefly Alpha

Firefly Aerospace|US
Operational
Payload LEO1,030 kg
Payload GTO--
Height29 m
Cost$15M
Reliability71.4% (5/7)
2-StageRP-1

A small launch vehicle designed for dedicated small satellite missions. Uses tap-off cycle engines with carbon fiber composite structures. Also developing the medium-lift MLV in partnership with Northrop Grumman.

Ceres-1

Galactic Energy|CN
Operational
Payload LEO400 kg
Payload GTO--
Height20 m
Cost$5M
Reliability86.7% (13/15)
4-StageSolid

China's leading commercial small launch vehicle from Galactic Energy. One of the first privately developed Chinese rockets to reach orbit. Provides cost-effective dedicated small-sat access to SSO.

Electron

Rocket Lab|US
Operational
Payload LEO300 kg
Payload GTO--
Height18 m
Cost$7.5M
Reliability91.1% (51/56)
2-StageRP-1

The leading dedicated small-satellite launcher. Uses electric turbopump-fed engines and carbon composite structure. Rocket Lab has demonstrated helicopter-based mid-air first stage recovery attempts to enable partial reuse.