Expendable space launch systems

expendable system for launching satellites, developed by the Indian Space Research Organisation

family of space-launch vehicles

family of Indian satellite launch vehicles

The Launch Vehicle Mark-3 or LVM3 (previously referred as the GSLV Mk III) is a three-stage medium-lift launch vehicle developed by the Indian Space Research Organisation (ISRO). Primarily designed to launch communication satellites into geostationary orbit, it is also due to launch crewed missions under the Indian Human Spaceflight Programme. LVM3 has a higher payload capacity than its predecessor, GSLV.

launch vehicle produced by Northrop Grumman from the United States

Iranian satellite rocket

two-stage orbital launch vehicle

small-lift launch vehicle produced by Israel from 1982 onwards

right|270px|thumb|The Liftoff of H-IIA Flight 19 right|270px|thumb|The H-IIA rocket lineup thumb|80px|The H-IIA thumb|right|Engine at Miraikan

The H-II (H2) rocket was a Japanese satellite launch system, which flew seven times between 1994 and 1999, with five successes. It was developed by NASDA in order to give Japan a capability to launch larger satellites in the 1990s. It was the first two-stage liquid-fuelled rocket Japan made using only technologies developed domestically. It was superseded by the H-IIA rocket following reliability and cost issues.

air-launched rocket

five-stage solid propellant rocket

The H-IIB (H2B) was a Japanese expendable launch system jointly developed by JAXA and Mitsubishi Heavy Industries. It was used exclusively to launch the H-II Transfer Vehicle (HTV, or Kōnotori) cargo spacecraft to the International Space Station.

rocket for launching satellites

Japanese satellite launch rocket

space launch vehicle that is expended after use

family of American rockets

Japanese expendable launch system

Start-1 is a Russian satellite launch vehicle based on the RT-2PM Topol, a Soviet intercontinental ballistic missile developed by Moscow Institute of Thermal Technology.

Indian small-lift launch vehicle

The Unha () is a North Korean expendable carrier rocket, which partially utilizes the same delivery system as the Taepodong-2 orbital launch system.

The VLS-1 () was the Brazilian Space Agency's main satellite launch vehicle. The launch vehicle would have been capable of launching satellites into orbit. The launch site was located at the Alcântara Launch Center due to its proximity to the equator.

two-stage solid-fueled booster rocket developed by the U.S. Air Force

space launch vehicle program of the United States Space Force

second version of SpaceX's Falcon 9 orbital launch vehicle

two-stage small launch vehicle by Isar Aerospace

family of Russian rocket upper stages

rocket family

Rus-M () was a proposed launcher design which was intended to become Russia's main launch vehicle for crewed spaceflight after 2018, and an integral part of the Orel spacecraft being developed to replace the Soyuz.

first member of the Falcon 9 launch vehicle family

Space launch vehicle Shtil' (Russian: Штиль - calm (weather)), is a converted SLBM used for launching artificial satellites into orbit, with a payload of around . It is the first launch vehicle to successfully launch a payload into orbit from a submarine, although launch from land based structures is possible as well.

family of British research ballistic missiles

proposed three-stage Launch vehicle

used as the upper stage for Soyuz-Ikar

Japanese private small-lift orbital rocket

canceled American launch vehicle

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world's first privately funded commercial rocket, produced from Minuteman I stages

space launch vehicle in development

rocket upper stage designed in Russia

cancelled Spanish launch vehicle

Russian superheavy launch space rocket

Shuttle-Centaur was a version of the Centaur upper stage rocket designed to be carried aloft inside the Space Shuttle and used to launch satellites into high Earth orbits or probes into deep space. Two variants were developed: Centaur G-Prime, which was planned to launch the Galileo and Ulysses robotic probes to Jupiter, and Centaur G, a shortened version planned for use with United States Department of Defense Milstar satellites and the Magellan Venus probe. The powerful Centaur upper stage allowed for heavier deep space probes, and for them to reach Jupiter sooner, prolonging the operational

family of launch vehicles developed by Astra

rocket

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low-cost launch vehicle concept