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A Guide to 2025’s Operational Orbital Rockets

Introduction

The global orbital launch landscape of 2025 is defined by an unprecedented operational tempo and a technological transformation. The sheer number of launches is driven primarily by the ongoing deployment of satellite mega-constellations, which demand frequent and affordable access to space. This sustained demand has created a market that not only justifies but actively funds the development of reusable rocket technology, a paradigm once considered science fiction but now the benchmark for competitiveness. This shift has reshaped the industry, creating an intense rivalry between established national space agencies and a new generation of agile commercial providers.

This environment is forcing every spacefaring power to recalibrate its strategy. The United States fosters a dynamic public-private ecosystem, while China pursues a state-guided commercial revolution to build its own constellations and secure its digital sovereignty. Europe, after a temporary gap in capability, is reasserting its strategic autonomy with a new family of launchers. Meanwhile, legacy powers like Russia are working to modernize their fleets, and nations like India and Japan are carving out niches with cost-effective, reliable, and technologically advanced vehicles. This article provides a detailed guide to the operational orbital rockets of 2025, organized by the major national and commercial players shaping this new era of spaceflight.

Nation/Provider Rocket Primary Role Payload to LEO (kg) Reusable
United States (SpaceX) Falcon 9 Crew, Cargo, Constellation, Commercial 17,500 Partial (Booster & Fairing)
United States (SpaceX) Falcon Heavy Heavy National Security, Interplanetary ~30,000 Partial (Boosters & Fairing)
United States (SpaceX) Starship Super Heavy Lift, Moon/Mars Missions 150,000 Full (Planned)
United States (ULA) Vulcan Centaur Heavy National Security, Commercial 27,200 No
United States (Rocket Lab) Electron Small Satellite Launch 320 Partial (Booster, Experimental)
China (CASC) Long March 2F Crew Transport (Shenzhou) 8,400 No
China (CASC) Long March 5B Space Station Modules 25,000 No
China (LandSpace) Zhuque-2 Commercial Medium Lift 6,000 No
Europe (Arianespace) Ariane 64 Heavy Commercial, Institutional 21,600 No
Europe (Arianespace) Vega-C Small/Medium Satellite Launch 3,300 No
Russia (Roscosmos) Soyuz-2 Crew & Cargo (ISS), Commercial ~8,200 No
Russia (Roscosmos) Angara A5 Heavy Lift, Military 24,500 No
India (ISRO) LVM3 Heavy Lift, Crew (Gaganyaan) 8,000 No
India (ISRO) PSLV Versatile Medium Lift, Interplanetary 3,800 No
Japan (JAXA/MHI) H3 Commercial, Institutional ~4,000+ No

The United States: A Diverse Ecosystem of Launch Providers

The American launch industry in 2025 is a study in contrasts, characterized by the market-defining dominance of SpaceX, the steadfast reliability of United Launch Alliance (ULA) for the nation’s most critical assets, and a vibrant, competitive small-launch sector. This diverse ecosystem is the result of a deliberate strategy of public-private partnerships that has accelerated innovation and driven down costs.

NASA’s Space Launch System: The Artemis Powerhouse

The Space Launch System (SLS) is NASA‘s super heavy-lift rocket, designed as the foundational transportation element for the Artemis program. As the most powerful rocket currently in operation, its primary purpose is to launch the Orion crew capsule, astronauts, and large cargo payloads on a single mission to the Moon and, eventually, to Mars. Developed as a successor to the Space Shuttle, the SLS incorporates proven hardware, including its main engines and solid rocket boosters, to ensure reliability for deep space human exploration.

The SLS is designed to be evolvable, with different configurations or “blocks” planned to support increasingly ambitious missions over time. Every version of the rocket is built around its massive core stage, which stands 212 feet tall and holds 733,000 gallons of super-cooled liquid hydrogen and liquid oxygen propellant.

Core Stage and Propulsion

The core stage is powered by four RS-25 engines, the same model that served as the main engines for the Space Shuttle fleet. For the SLS, these engines have been upgraded with new controllers and are pushed to operate at a higher thrust level, collectively providing about 2 million pounds of thrust.

The majority of the rocket’s power at liftoff comes from two five-segment solid rocket boosters (SRBs) strapped to the sides of the core stage. These are stretched versions of the four-segment boosters used for the Shuttle. Each SRB is 177 feet tall, weighs 1.6 million pounds, and produces a maximum of 3.6 million pounds of thrust. Together, the twin boosters provide more than 75% of the total vehicle thrust during the first two minutes of flight.

Block Configurations and Upper Stages

The SLS is designed with a modular, evolvable architecture to support a variety of missions.

  • Block 1: This is the initial configuration of the SLS, standing 322 feet tall and producing 8.8 million pounds of thrust at liftoff. It is capable of sending over 27 metric tons (59,500 lbs) on a trajectory to the Moon. This version uses the Interim Cryogenic Propulsion Stage (ICPS), a modified upper stage from the Delta IV rocket powered by a single RL10 engine, to perform the final burn that sends Orion out of Earth’s orbit and toward the Moon. The Block 1 configuration was used for the successful Artemis I mission and is planned for Artemis II and III.
  • Block 1B: Planned to debut with the Artemis IV mission, the Block 1B enhances the rocket’s capability by introducing the Exploration Upper Stage (EUS). The EUS is a much larger and more powerful upper stage, equipped with four RL10 engines. This upgrade increases the rocket’s payload capacity to over 38 metric tons (83,700 lbs) in its crew configuration, allowing it to launch the Orion spacecraft and large, co-manifested cargo like modules for the lunar Gateway station on a single flight.
  • Block 2: The final and most powerful planned version of the SLS, Block 2 will replace the shuttle-derived SRBs with advanced boosters, increasing the total liftoff thrust to 9.5 million pounds. This configuration will be the workhorse for delivering the heaviest cargo needed for a sustained human presence on the Moon and for future crewed missions to Mars, with the ability to lift over 46 metric tons (101,400 lbs) to deep space.
Configuration Height Max Thrust Payload to Trans-Lunar Injection Upper Stage
Block 1 98 m (322 ft) 39 MN (8.8M lbf) >27,000 kg ICPS
Block 1B 111 m (365 ft) 40 MN (8.9M lbf) ~42,000 kg EUS
Block 2 111 m (365 ft) 42 MN (9.5M lbf) >46,000 kg EUS

SpaceX: The Pace-Setter of the New Space Age

SpaceX is not merely a launch provider; it is the primary force reshaping the economics and operational cadence of space access worldwide. Its mastery of reusability has enabled a launch frequency that was unimaginable a decade ago, allowing it to capture the majority of the global launch market.

Falcon 9

The Falcon 9 Block 5 is the undisputed workhorse of the global launch industry. In 2025, it is responsible for the lion’s share of orbital launches, serving a diverse manifest that includes deploying its own Starlink internet satellites, launching commercial communications satellites, executing cargo resupply (CRS) and science missions for NASA, and flying sensitive national security payloads for the National Reconnaissance Office (NRO) and U.S. Space Force.

The rocket’s defining feature is its operational reusability. The first-stage booster, after powering the ascent, performs a series of engine burns to return to Earth, landing either on an autonomous droneship at sea or back at a landing zone near the launch site. The payload fairing halves are also regularly recovered and reflown. This capability is no longer experimental; it is a routine and highly reliable part of every mission. The flight heritage of the fleet is extensive, with one booster, B1067, achieving its 27th flight in April 2025, a testament to the system’s robustness. This reusability is more than a cost-saving measure; it is a strategic multiplier. By dramatically reducing the need to manufacture a new first stage for every flight, SpaceX has shattered the traditional production bottleneck that limits launch rates. This enables a rapid launch cadence, with flights sometimes occurring just days apart from the same launch pad. This operational tempo gives SpaceX an unmatched ability to serve the high-demand markets for satellite constellation deployment and frequent rideshare missions, generating a vast amount of flight data. This data, in turn, fuels a continuous cycle of refinement and reliability improvements, further widening the gap with competitors who fly less often and must build a new rocket for each mission.

The Falcon 9 is also one of only two operational American rockets certified to carry humans. Paired with the Crew Dragon capsule, it regularly transports NASA and international astronauts to the International Space Station (ISS). It also serves the growing private human spaceflight market, as demonstrated by the Fram2 mission in April 2025, the first crewed flight to a polar orbit.

Technologically, the Falcon 9 is a two-stage rocket fueled by rocket-grade kerosene (RP-1) and liquid oxygen (LOX). The first stage is powered by nine Merlin 1D engines arranged in an “Octaweb” configuration, while the second stage uses a single Merlin engine optimized for the vacuum of space.

Falcon Heavy

For the heaviest payloads, SpaceX operates the Falcon Heavy. Architecturally, it consists of a strengthened Falcon 9 center core flanked by two standard Falcon 9 first stages acting as side boosters. At liftoff, its 27 Merlin 1D engines generate over 5 million pounds of thrust, making it one of the most powerful operational rockets in the world.

Its primary purpose is to launch payloads that are too massive or require too much energy for a Falcon 9. This includes large national security satellites for the Department of Defense, heavy commercial geosynchronous satellites, and interplanetary science missions that need to be sent on high-energy trajectories toward the Moon, Mars, or beyond. Like its smaller sibling, the Falcon Heavy is partially reusable. Following separation, the two side boosters perform synchronized return maneuvers and land back at Cape Canaveral. The center core, which burns for longer and travels to a higher altitude, can also be recovered on a droneship, though this is often expended to maximize payload performance.

Starship

Starship represents SpaceX’s next great ambition: a fully and rapidly reusable, two-stage, super-heavy-lift launch system. It is designed to eventually replace the Falcon family and enable large-scale missions to Earth orbit, the Moon, and Mars.

The system consists of the Super Heavy booster, powered by 33 Raptor engines, and the Starship upper stage, which serves as both the second stage and the in-space vehicle, powered by six Raptor engines. Both stages are designed to return to the launch site for rapid reuse. A key technological shift is the use of sub-cooled liquid methane (methalox) as propellant, which is more efficient, cleaner-burning, and can potentially be produced on Mars. For deep space missions, Starship is designed to be refueled in orbit by a tanker variant, allowing it to transport up to 150 metric tons of payload to the Moon or Mars.

As of 2025, Starship is in an aggressive flight testing phase from its Starbase facility in Texas. While some early test flights have ended in failure, each launch provides crucial data for iterative design improvements. NASA has selected a modified version of Starship as the Human Landing System (HLS) that will return astronauts to the lunar surface for the Artemis program.

Vehicle Height Diameter Stages Propellant Liftoff Thrust Payload to LEO (Reusable) Payload to GTO (Reusable) Reusability
Falcon 9 70 m 3.7 m 2 LOX / RP-1 7,607 kN ~17,500 kg ~5,500 kg Booster, Fairing
Falcon Heavy 70 m 12.2 m (width) 2 LOX / RP-1 22,819 kN ~30,000 kg ~8,000 kg Side Boosters, Center Core (mission dependent), Fairing
Starship 123 m 9 m 2 Liquid Methane / LOX ~75,900 kN 100,000 – 150,000 kg 100,000+ kg (with refueling) Fully Reusable (Booster & Ship)

United Launch Alliance (ULA): The Standard for Mission Assurance

For two decades, United Launch Alliance has been the custodian of America’s most critical space missions, building a reputation for unparalleled reliability. In 2025, ULA is in the midst of a strategic transition, phasing out its legacy rockets and introducing the Vulcan Centaur to compete in a new market landscape.

Atlas V

The Atlas V is a veteran of the U.S. launch fleet with a near-perfect success record, making it the go-to vehicle for high-value NASA science missions and classified national security payloads. Its modular design, denoted by a three-digit number (e.g., Atlas V 551), allows it to be configured for a wide range of mission requirements by varying the payload fairing size (4 m or 5 m), the number of solid rocket boosters (zero to five), and the number of engines on its upper stage (one or two).

The rocket’s first stage is powered by a single Russian-made RD-180 engine burning RP-1 and LOX, while its powerful Centaur upper stage uses a highly efficient liquid hydrogen and liquid oxygen (hydrolox) RL10 engine. The Atlas V is an expendable vehicle. In 2025, it is in the final phase of its operational life, with its remaining flights primarily dedicated to launching a portion of Amazon’s Project Kuiper internet constellation.

Vulcan Centaur

The Vulcan Centaur is ULA’s next-generation flagship, designed to replace both the Atlas V and the Delta IV Heavy with a single, more capable, and more affordable system. Its development represents a crucial strategic pivot for ULA. The Atlas V, while reliable, was becoming too expensive to compete commercially and its reliance on the Russian RD-180 engine became a significant geopolitical liability. To remain a key provider for the Department of Defense’s National Security Space Launch (NSSL) program, ULA needed a new, domestically powered, and more cost-effective rocket.

Vulcan is the result of that effort. After completing two certification flights, the rocket was fully certified by the U.S. Space Force in March 2025 to begin flying NSSL missions. Its manifest includes the upcoming USSF-106 mission for the Space Force, the first cargo flight of Sierra Space’s Dream Chaser spaceplane to the ISS, and a large contract for 38 launches for Amazon’s Project Kuiper.

Technologically, Vulcan marks a significant evolution from its predecessors. Its first stage is powered by two BE-4 engines, built by Blue Origin, which use liquid methane and LOX. This ends ULA’s dependence on foreign propulsion systems. For additional thrust, it can be fitted with up to six GEM 63XL solid rocket boosters. Its upper stage is the Centaur V, a powerful and upgraded version of the venerable Centaur stage, powered by two RL10 engines. This new architecture reflects a broader U.S. space policy aimed at ensuring at least two independent and reliable domestic launch providers for national security, fostering a resilient industrial base and preventing a monopoly.

Vehicle Height Diameter Stages Propellant (Stage 1 / Stage 2) Liftoff Thrust (Max) Payload to LEO (kg) Payload to GTO (kg)
Atlas V Up to 62.2 m 3.81 m 2 LOX / RP-1 / LH2 / LOX ~12,141 kN 18,850 8,900
Vulcan Centaur Up to 67.3 m 5.4 m 2 Liquid Methane / LOX / LH2 / LOX ~17,056 kN 27,200 14,500

Northrop Grumman: Specialized Launch Solutions

Northrop Grumman occupies a specialized niche in the U.S. launch market, providing essential ISS cargo services with its Antares rocket and tailored launch solutions for government clients with its Minotaur family of solid-fuel rockets.

Antares

The primary mission of the Antares rocket is the launch of the Cygnus cargo spacecraft to the International Space Station under NASA‘s Commercial Resupply Services (CRS) contract. The Antares 230+ series, which concluded its service in 2023, was notable for its international supply chain, featuring a first stage manufactured in Ukraine by Pivdenne and Pivdenmash, and powered by two Russian-made RD-181 engines.

Due to geopolitical events disrupting this supply chain, Northrop Grumman is partnering with Firefly Aerospace to develop the Antares 300 series. This upgraded version will feature a new first stage built by Firefly, ensuring the continuation of Cygnus missions from the Wallops Flight Facility in Virginia. The first flight of the Antares 330 is planned for mid-2025.

Minotaur Family

The Minotaur family of launchers (Minotaur I, IV, V, and C) is unique in that it is built using decommissioned solid rocket motors from the U.S. Air Force’s Minuteman and Peacekeeper intercontinental ballistic missile (ICBM) programs. This heritage makes them a cost-effective solution for specific government needs.

These solid-fuel rockets are used exclusively for launching U.S. government payloads, primarily for the Department of Defense, the NRO, and the Space Force. They provide a responsive launch capability for smaller satellites. In April 2025, a Minotaur IV successfully launched the NROL-174 mission from Vandenberg Space Force Base in California.

Vehicle Height Diameter Propellant Primary Mission Payload to LEO (kg)
Antares 230+ (Retired) 42.5 m 3.9 m Liquid (Stage 1) / Solid (Stage 2) ISS Cargo (Cygnus) 8,000
Antares 330 (Planned) ~47.0 m ~3.0 m Liquid (Stage 1) / Solid (Stage 2) ISS Cargo (Cygnus) 10,800
Minotaur I 19.2 m 1.27 m Solid Small Government Satellites 580
Minotaur IV 23.9 m 2.34 m Solid Medium Government Satellites 1,735

America’s Small Launch Vanguard

The proliferation of small satellites for communications, Earth observation, and technology demonstration has created a dedicated market for smaller, more agile launch vehicles. Several American companies are competing in this dynamic sector.

Rocket Lab Electron

Rocket Lab‘s Electron is the clear leader in the dedicated small satellite launch market, having established a record of reliability and a high launch cadence that rivals many larger vehicles. The Electron is a two-stage rocket known for its innovative technologies, including a lightweight carbon-composite structure and its nine unique Rutherford engines on the first stage. The Rutherford is the first electric pump-fed engine to power an orbital rocket, using batteries to drive its turbopumps instead of a traditional gas generator cycle.

The rocket often flies with an optional third stage, the Photon kick stage, which is capable of multiple engine burns. This gives Electron the ability to deliver small satellites to precise orbits with high accuracy and even to perform interplanetary missions, such as NASA’s CAPSTONE mission to the Moon. The company is also actively developing methods to recover and reuse its first stage, having successfully demonstrated both ocean splashdowns and mid-air recovery attempts with a helicopter. In 2025, Electron continues to fly a busy manifest for a mix of commercial and government customers, including NASA and the NRO.

Firefly Aerospace Alpha

Firefly Aerospace is an emerging competitor in the small-to-medium launch market with its Alpha rocket. The vehicle features an all-carbon-fiber composite body, designed to be lightweight and strong, and is powered by four Reaver engines on its first stage, which burn RP-1 and LOX.

While the Alpha rocket is operational, its early flight history has included some failures, which is a common challenge in maturing a new launch vehicle. A launch in April 2025 for a Lockheed Martin demonstration mission failed to reach orbit. Despite these setbacks, Firefly continues to secure contracts and is a key partner for Northrop Grumman in developing the new first stage for the Antares 300 rocket.

Provider Vehicle Height Diameter Propellant Payload to LEO (kg) Payload to SSO (kg)
Rocket Lab Electron 18 m 1.2 m LOX / RP-1 320 200
Firefly Aerospace Alpha 29 m 1.8 m LOX / RP-1 630 ~400

China: A Nation’s Rapid Ascent

China’s space program in 2025 is characterized by a powerful dual-pronged strategy. The state-owned China Aerospace Science and Technology Corporation (CASC) operates the venerable Long March family of rockets, providing the foundational capability for all major national missions. In parallel, a vibrant and rapidly growing commercial sector, guided by state policy, is developing a new generation of low-cost and reusable launchers to serve emerging markets and strategic national projects.

The Long March Family: The State’s Foundational Fleet

The Long March series is the backbone of China’s space ambitions, responsible for everything from crewed missions and space station construction to deep space exploration.

  • Long March 2F: This is China’s human-rated launch vehicle, distinguished by its launch escape system and an impeccable reliability record. Its sole purpose is to launch the Shenzhou spacecraft, carrying taikonauts to and from the Tiangong space station.
  • Long March 5: As China’s heavy-lift rocket, the Long March 5 is essential for the nation’s most ambitious projects. The Long March 5B variant, with its massive payload fairing, was used to launch the large modules of the Tiangong space station. The standard Long March 5 has launched deep space missions, including the Chang’e lunar sample return probes and the Tianwen-1 orbiter and rover to Mars. It features a modern cryogenic core stage using liquid hydrogen and liquid oxygen (LH2/LOX), supplemented by four large kerosene-fueled boosters.
  • Long March 7: This medium-lift rocket is a key part of China’s plan to modernize its fleet. It uses more environmentally friendly RP-1 and LOX propellants, replacing older launchers that used toxic hypergolic fuels. Its primary mission is launching the Tianzhou automated cargo craft to resupply the Tiangong space station.
  • Other Operational Variants: The Long March family is extensive, with numerous other variants in active service in 2025. These include the workhorse Long March 2D, the geosynchronous mission specialist Long March 3B/E, and the versatile Long March 6A, all of which continue to fly frequently for various satellite deployment missions.

The Rise of Commercial Chinese Launch

The emergence of a dynamic commercial launch sector in China is not a purely free-market phenomenon but a deliberate national strategy. Recognizing the need for a high-cadence, low-cost launch capability to deploy its own satellite mega-constellations—such as Guowang and Thousand Sails—the Chinese government opened the sector to private investment. This created a guaranteed customer base for new companies, fostering a competitive domestic market designed to build a resilient launch ecosystem that can rival Western counterparts. This strategy allows the state-owned CASC to focus on high-priority national missions while the commercial sector provides the high-volume access to LEO required for strategic projects. In 2025, these commercial companies are becoming increasingly integrated into the national space program, with some winning contracts to launch cargo to the Tiangong space station.

  • LandSpace Zhuque-2: LandSpace made history when its Zhuque-2 became the world’s first methane-fueled rocket to successfully reach orbit, a significant milestone for the global space industry. The rocket, which uses liquid methane and LOX, is now operational with its upgraded Zhuque-2E variant flying commercial payloads. The company is also developing the larger, reusable Zhuque-3.
  • Galactic Energy Ceres-1: The Ceres-1 is a prolific four-stage solid-fuel rocket that has become a workhorse for the Chinese commercial small satellite market. It has established a strong record of successful launches from both land-based pads at Jiuquan and mobile sea platforms.
  • CAS Space Kinetica-1 (Lijian-1): Developed by a commercial spin-off of the Chinese Academy of Sciences, the Kinetica-1 is currently China’s most powerful solid-fuel rocket. This four-stage vehicle is capable of launching payloads over 1,500 kg to sun-synchronous orbit (SSO).
  • i-Space Hyperbola-1: i-Space was the first private Chinese company to reach orbit with its Hyperbola-1 rocket in 2019. This four-stage solid-fuel launcher has had a mixed reliability record since its debut but remains an active part of the commercial landscape.
Operator Vehicle Propellant Primary Mission Payload to LEO (kg) Reusable
CASC Long March 2F N2O4 / UDMH Crew Transport (Tiangong) 8,400 No
CASC Long March 5B LH2 / LOX & LOX / RP-1 Space Station Modules 25,000 No
CASC Long March 7 LOX / RP-1 Cargo Transport (Tiangong) 13,500 No
LandSpace Zhuque-2E Liquid Methane / LOX Commercial Medium Lift 6,000 No
Galactic Energy Ceres-1 Solid / Liquid (Upper Stage) Commercial Small Satellites 400 No
CAS Space Kinetica-1 Solid Commercial Small/Medium Lift 2,000 No
i-Space Hyperbola-1 Solid / Liquid (Attitude Control) Commercial Small Satellites ~300 No

Europe: Unifying for Autonomous Space Access

For Europe, 2025 marks a critical year of recovery and reassertion. The retirement of the venerable Ariane 5, coupled with launch failures and delays affecting its Vega-C light launcher and the loss of access to Russian Soyuz rockets, left the continent temporarily without independent launch capability. This created a significant strategic vulnerability, forcing reliance on American providers like SpaceX for critical launches. The successful operational debut of Ariane 6 and the return-to-flight of Vega-C are therefore driven by a powerful imperative: ensuring Europe’s strategic autonomy and sovereign access to space. This goal underpins the design and operation of its new generation of launchers, managed by the European Space Agency (ESA) and operated commercially by Arianespace.

Ariane 6

Ariane 6 is Europe’s new-generation heavy-lift launcher, designed as a more versatile and cost-effective successor to the highly reliable Ariane 5. Its design is fundamentally modular, allowing it to be tailored to specific mission needs. It comes in two configurations:

  • Ariane 62: Uses two solid rocket boosters and is optimized for lighter payloads, such as government science missions or single commercial satellites, lifting up to 10.3 tonnes to LEO.
  • Ariane 64: Uses four solid rocket boosters for maximum performance, capable of launching heavy payloads up to 21.6 tonnes to LEO or placing two large telecommunications satellites into geostationary transfer orbit (GTO) simultaneously.

The rocket’s first stage, the Lower Liquid Propulsion Module (LLPM), is powered by a single Vulcain 2.1 engine, an upgraded and more cost-efficient version of the engine used on Ariane 5, burning liquid hydrogen and liquid oxygen. The solid rocket boosters are the P120C model, which are also used as the first stage of the Vega-C rocket. This parts-sharing strategy is a key element of the program’s effort to reduce production costs by increasing manufacturing volume.

A significant advancement is the new Vinci engine on the upper stage. It is also fueled by hydrolox and can be re-ignited multiple times in space. This capability allows for complex mission profiles, such as deploying satellites into different orbits on a single flight. It also enables the upper stage to perform a final de-orbit burn, directing it to burn up in the atmosphere over an unpopulated area and mitigating the creation of space debris. After a successful maiden flight in 2024, Ariane 6 conducted its first commercial launch in March 2025, and its order book is full with both European institutional and international commercial customers.

Vega-C

The Vega-C is Europe’s upgraded light-lift launcher, offering significantly more performance and volume than its predecessor, the original Vega. In 2025, Vega-C is fully operational again after a previous launch failure, successfully launching ESA‘s Biomass Earth observation satellite in April.

The rocket is a four-stage vehicle. The first stage is the same P120C solid motor used as a booster on Ariane 6. The second and third stages, the Zefiro-40 and Zefiro-9, are also solid-propellant motors. The fourth and final stage is the liquid-fueled Attitude Vernier Upper Module (AVUM+). This upper stage uses hypergolic propellants and can be restarted up to seven times, giving it exceptional flexibility to deliver multiple small satellites to different orbits with high precision.

Vega-C is designed to serve the growing market for small to medium-sized satellites. It can accommodate a wide variety of payloads using its Small Spacecraft Mission Service (SSMS) dispenser, which is a modular adapter capable of carrying dozens of small satellites on a single rideshare mission.

Vehicle Height Diameter Stages Propellant (Core / Boosters) Liftoff Thrust (Max) Payload to LEO (kg) Payload to GTO/SSO (kg)
Ariane 62 ~60 m 5.4 m 2 LH2 / LOX / Solid ~10,570 kN 10,300 4,500 (GTO)
Ariane 64 ~60 m 5.4 m 2 LH2 / LOX / Solid ~19,570 kN 21,600 11,500 (GTO)
Vega-C 35 m 3.4 m 4 Solid / Liquid (Upper Stage) ~4,500 kN 3,300 2,300 (SSO)

Russia: A Legacy Power in Transition

The Russian space program in 2025 continues to rely heavily on its legendary Soviet-era launch systems while slowly working to introduce a new generation of modern, domestically-produced rockets. The state corporation Roscosmos operates a fleet that, while aging, remains a critical capability for maintaining the International Space Station and launching the nation’s military satellites.

The Soyuz Family

The Soyuz rocket is the most-flown launch vehicle in history, a direct descendant of the R-7 missile that launched Sputnik. In 2025, the modernized Soyuz-2 family (with variants 2.1a, 2.1b, and the lighter 1v) remains Russia’s primary launcher. Its most prominent role is serving the International Space Station. The Soyuz-2.1a variant is used to launch the Soyuz MS spacecraft, which carries crews to the station, and the automated Progress MS cargo vehicles for resupply missions.

The rocket’s design is iconic, featuring four tapering liquid-fueled boosters that surround a central core stage, a configuration known as the “Korolev Cross.” Both the boosters and the core stage burn RP-1 and LOX. Despite its age, the Soyuz remains one of the world’s most reliable launch systems.

The Angara Family

The Angara rocket family is Russia’s long-planned replacement for several legacy launchers, most notably the heavy-lift Proton. A key driver for its development is strategic: Angara is designed to be launched from Russian territory at the Plesetsk and Vostochny Cosmodromes, ending Russia’s reliance on the Baikonur Cosmodrome in Kazakhstan for heavy-lift missions.

The family is modular, built around a common building block called the Universal Rocket Module (URM-1), which is powered by a modern RD-191 engine burning RP-1 and LOX. This is a significant improvement over the toxic hypergolic propellants used by Proton. Two variants are currently operational:

  • Angara 1.2: A light-lift version consisting of a single URM-1 first stage and a second stage.
  • Angara A5: A heavy-lift version that uses a central URM-1 core stage augmented by four additional URM-1s as strap-on boosters.

While operational, the Angara family has a very low flight rate. As of 2025, it has flown only a handful of missions, primarily for the Russian Ministry of Defence.

Proton-M

The Proton-M is a powerful heavy-lift rocket with a long heritage stretching back to the Soviet era. For decades, it was Russia’s primary vehicle for launching large government and commercial satellites to geostationary orbit. However, the rocket is now being phased out. Its use of highly toxic hypergolic propellants makes it environmentally hazardous and costly to operate, and its launches are tied to the Baikonur Cosmodrome. Only a few final flights of the Proton-M are planned as its missions are transitioned to the Angara A5.

Vehicle Height Propellant Primary Mission Payload to LEO (kg) Payload to GTO (kg)
Soyuz-2.1a/b ~46 m LOX / RP-1 ISS Crew & Cargo, Government ~8,200 ~3,250
Angara 1.2 ~42.7 m LOX / RP-1 Light/Medium Government Satellites 3,800
Angara A5 ~55 m LOX / RP-1 Heavy Government Satellites 24,500 ~5,400 (Briz-M)
Proton-M ~58 m N2O4 / UDMH Heavy Lift (Retiring) 23,000 ~6,300

India: A Strategic and Self-Reliant Space Power

The Indian Space Research Organisation (ISRO) has cultivated a diverse and highly self-reliant launch capability. Its fleet is strategically designed with a tiered approach, featuring dedicated vehicles for small, medium, and heavy payloads, enabling India to meet all of its domestic needs while also competing in the international launch market.

PSLV (Polar Satellite Launch Vehicle)

The Polar Satellite Launch Vehicle, or PSLV, is the celebrated workhorse of the Indian space program. It has earned a reputation for exceptional reliability and versatility over dozens of successful flights. Its primary mission is launching India’s remote sensing satellites into polar and sun-synchronous orbits, but its capabilities extend far beyond that. The PSLV was responsible for India’s most prestigious interplanetary missions, including the Chandrayaan-1 lunar orbiter and the Mars Orbiter Mission (Mangalyaan).

The PSLV is a four-stage rocket that uses an alternating combination of solid and liquid-fueled stages. It comes in several configurations—Core Alone (CA), QL, and XL—which are distinguished by the number of solid strap-on boosters (zero, four, or six, respectively) used to augment the first stage’s thrust.

GSLV and LVM3 (Launch Vehicle Mark 3)

To achieve self-reliance in launching heavy communications satellites to geostationary orbit, ISRO developed the Geosynchronous Satellite Launch Vehicle (GSLV) family. The culmination of this effort is the Launch Vehicle Mark 3 (LVM3), India’s most powerful and advanced rocket.

The LVM3 is a three-stage rocket featuring two massive S200 solid strap-on boosters, a liquid-fueled core stage powered by two Vikas engines, and a domestically developed high-thrust cryogenic upper stage. It has successfully flown all of its missions, including the Chandrayaan-2 and Chandrayaan-3 missions to the Moon. Crucially, the LVM3 has been human-rated and is the designated launch vehicle for India’s inaugural crewed spaceflight program, Gaganyaan.

SSLV (Small Satellite Launch Vehicle)

The Small Satellite Launch Vehicle (SSLV) is ISRO’s newest rocket, developed to specifically target the booming global market for small satellite launches. It is designed for low cost, flexibility in accommodating multiple payloads, and a quick turnaround time, enabling a “launch-on-demand” capability that is highly attractive to commercial customers.

The SSLV is a four-stage vehicle. The first three stages use solid propellants, while the fourth stage is a liquid-fueled Velocity Trimming Module (VTM) that precisely injects the satellites into their desired orbits. Following its successful developmental flights, ISRO is in the process of transferring the production and operation of the SSLV entirely to the Indian private industry, a landmark step in the commercialization of the country’s space sector.

Vehicle Height Lift-off Mass Stages Primary Mission Payload to LEO (kg) Payload to GTO/SSO (kg)
SSLV 34 m 120 t 3 + liquid trim stage Commercial Small Satellites 500 300 (SSO)
PSLV-XL 44 m 320 t 4 Medium Lift, Remote Sensing, Interplanetary 3,800 1,750 (SSO)
GSLV Mk II ~51 m 415 t 3 Geosynchronous Satellites 5,000 2,500 (GTO)
LVM3 43.5 m 640 t 3 Heavy Lift, Crewed Missions (Gaganyaan) 8,000 4,000 (GTO)

Japan: A Tradition of Precision and Advanced Technology

Japan’s space program, led by the Japan Aerospace Exploration Agency (JAXA) and its industrial partner Mitsubishi Heavy Industries (MHI), has a long history of technological excellence and high reliability. In 2025, its launch efforts are centered on its new flagship rocket, the H3, which is designed to be more competitive in the global commercial market.

H3

The H3 is the direct successor to Japan’s highly reliable but expensive H-IIA and H-IIB rockets. Its development was driven by the need for a launch vehicle that maintains Japan’s reputation for quality while being significantly cheaper to build and operate. The Japanese strategy for achieving this cost reduction is not centered on the disruptive reusability pioneered by SpaceX, but rather on a classic model of industrial and manufacturing excellence. The H3’s design was simplified, reducing the total number of components by 20% and incorporating advanced manufacturing techniques like 3D printing and automation drawn from the automotive industry. This approach bets that for many high-value satellite customers, proven reliability and precise schedule assurance remain paramount.

A key technological innovation of the H3 is its new LE-9 first-stage engine. It is the first rocket in the world to use an expander bleed cycle—a highly efficient and reliable engine design—for its main stage propulsion. The rocket is modular, allowing its configuration to be adapted to different mission requirements. The number of LE-9 engines on the first stage (two or three) and the number of solid rocket boosters (zero, two, or four) can be varied. This flexibility allows the H3 to launch a wide range of payloads to various orbits.

After a failure on its maiden flight in 2023, the H3 returned to flight successfully and is fully operational in 2025. It has conducted several missions, including the launch of the QZS-6 navigation satellite for Japan’s own regional GPS-like system.

Configuration Height Boosters First Stage Engines Payload to LEO (kg) Payload to GTO (kg)
H3-30S 63 m 0 3 ~4,000 ~2,100
H3-22S/L 63 m / 69 m 2 2 4,000
H3-24L 69 m 4 2 ~7,900

South Korea: An Emerging Independent Space Power

South Korea is rapidly establishing itself as a significant and independent space power, driven by a national strategy to foster a robust, private-sector-led aerospace economy. The 2024 formation of the Korea AeroSpace Administration (KASA) signaled a decisive shift, aiming to integrate space capabilities into the country’s economic and national security goals. With a focus on developing advanced launch vehicles, a domestic satellite navigation system, and lunar exploration missions, South Korea is positioning itself as a key player in the global space landscape.

Nuri (KSLV-II): The National Workhorse

The Nuri, also known as KSLV-II, is the cornerstone of South Korea’s sovereign launch capability. Developed by the Korea Aerospace Research Institute (KARI), Nuri is a three-stage rocket powered entirely by domestically produced liquid-fueled engines. The rocket stands 47.2 meters tall and uses kerosene and liquid oxygen as its propellants. It is designed to place payloads of up to 1,900 kg into a 700-kilometer sun-synchronous orbit.

Following successful launches in 2022 and 2023, the Nuri is an active launch vehicle, with its fourth flight scheduled for late 2025. This upcoming mission marks a pivotal moment in the nation’s space strategy, as the private aerospace and defense company Hanwha Aerospace, which already manufactures the rocket’s engines, will assume the role of systems integrator. This technology transfer is a critical step in transitioning the Nuri program from a government-led project to a commercially operated one, with Hanwha expected to begin its own launch services by 2028.

The Commercial Frontier

Alongside the maturation of its national rocket, South Korea is cultivating a dynamic commercial space sector.

INNOSPACE HANBIT-Nano

A leading example of this new commercial drive is the HANBIT-Nano, a small satellite launch vehicle developed by the startup INNOSPACE. This two-stage rocket is notable for its innovative hybrid propulsion system. The first stage employs a 25-ton-thrust engine that uses solid paraffin-based fuel with a liquid oxygen oxidizer, while the second stage is powered by a 3-ton-thrust liquid methane engine. The HANBIT-Nano is scheduled to make its inaugural commercial launch in July 2025 from the Alcântara Space Center in Brazil, aiming to serve the growing global small satellite market.

Provider Vehicle Primary Mission Payload to SSO (kg) Propellant
KARI / Hanwha Aerospace Nuri (KSLV-II) Government & Commercial Satellites 1,900 Kerosene / LOX
INNOSPACE HANBIT-Nano Commercial Small Satellites ~90 Hybrid (Stage 1) / Methane (Stage 2)

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Summary

The state of orbital launch in 2025 is more dynamic and competitive than at any point in history. Several clear trends define the era.

The paradigm of reusability, once a bold experiment, is now the dominant force in the market. Led by SpaceX’s Falcon 9, the ability to recover and refly rocket boosters has fundamentally altered the economics of space access, enabling an unprecedented launch cadence that is now the benchmark against which all competitors are measured. Nations and companies are no longer debating if they should pursue reusability, but are actively developing their own systems to remain competitive.

The line between government and private spaceflight has become increasingly blurred. Commercial companies are now entrusted with launching national security satellites and flying astronauts, while state-led programs, particularly in China, are deliberately fostering private industry to build a more robust and layered national capability.

While facing similar market pressures, each major space power is pursuing a distinct strategy. The United States leverages a dynamic public-private partnership to spur innovation. China employs a state-guided model to rapidly build a commercial ecosystem that serves national strategic goals. Europe prioritizes sovereign access to space to ensure its strategic autonomy. Russia is focused on modernizing its legacy fleet, while India and Japan are carving out niches through cost-effective self-reliance and advanced manufacturing, respectively.

A technological shift in propulsion is underway. The operational success of the first methane-fueled orbital rocket and the development of powerful new methalox engines for vehicles like Starship and Vulcan signal the beginning of a move away from traditional propellants toward fuels that are cleaner, more efficient, and better suited for reuse.

Today, the field of operational launchers is more crowded than ever. From dedicated small satellite launchers to super-heavy-lift vehicles, the proliferation of capabilities from a growing number of countries and companies points to a future of even greater access to space, driven by a mix of national ambition and commercial competition.

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