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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
1,365
Total Launches
Status:
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Showing 24 of 24 launch vehicles

Starship / Super Heavy

In Development
Payload LEO150,000 kg
Payload GTO21,000 kg
Height121 m
Cost$10M
Reliability54.5% (6/11)
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 first demonstrated in October 2024. Block 3 upgrade vehicles in preparation for 2026 flights.

Falcon Heavy

Operational
Payload LEO63,800 kg
Payload GTO26,700 kg
Height70 m
Cost$97M
Reliability100.0% (11/11)
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

Operational
Payload LEO45,000 kg
Payload GTO13,000 kg
Height98 m
Cost$68M
Reliability100.0% (2/2)
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. Successfully landed its first stage booster on the second flight in November 2025.

Vulcan Centaur

ULA|US
Operational
Payload LEO27,200 kg
Payload GTO12,350 kg
Height61.6 m
Cost$110M
Reliability66.7% (2/3)
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
Reliability93.3% (14/15)
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% (5/5)
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% (104/115)
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

Operational
Payload LEO22,800 kg
Payload GTO8,300 kg
Height70 m
Cost$67M
Reliability99.5% (612/615)
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 134 flights in 2024 and 165 in 2025. Boosters have been certified for up to 40 flights each. Block 5 variant first flew May 2018 (original Falcon 9 v1.0 debuted June 2010).

Ariane 6

ArianeGroup|EU
Operational
Payload LEO21,650 kg
Payload GTO11,500 kg
Height56 m
Cost$77M
Reliability83.3% (5/6)
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. First A64 variant launched in February 2026 with Amazon Kuiper satellites.

Terran R

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
Reliability77.8% (7/9)
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. Suffered a second-stage anomaly on its December 2025 flight after five consecutive successes.

Neutron

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. Maiden flight expected in 2026 from Wallops Island, Virginia.

Long March 3B/E

CALT / CASC|CN
Operational
Payload LEO11,500 kg
Payload GTO5,500 kg
Height56.33 m
Cost$70M
Reliability95.9% (93/97)
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% (9/9)
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
Reliability97.3% (72/74)
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% (62/65)
4-StageHTPB

India's highly reliable workhorse launcher with over 65 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
Reliability99.0% (104/105)
2-StageUDMH

China's highly reliable medium-lift workhorse, primarily used for Earth observation and SSO missions. Reached its 100th mission milestone in September 2025, one of the most frequently launched Chinese vehicles.

Vega-C

Avio|EU
Operational
Payload LEO2,300 kg
Payload GTO--
Height34.8 m
Cost$37M
Reliability85.7% (6/7)
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 December 2024 after a two-year stand-down, completing four successful missions in 2025.

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

Operational
Payload LEO1,030 kg
Payload GTO--
Height29 m
Cost$15M
Reliability75.0% (6/8)
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
Reliability91.3% (21/23)
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

Operational
Payload LEO300 kg
Payload GTO--
Height18 m
Cost$7.5M
Reliability95.1% (77/81)
2-StageRP-1

The leading dedicated small-satellite launcher. Uses electric turbopump-fed engines and carbon composite structure. Rocket Lab achieved a record 21 Electron launches in 2025 with 100% mission success, cementing its position as the second most frequently launched US rocket.

Last updated March 2026