V-2 The V-2 ballistic missile (known to its designers as the A4) was the world's first operational liquid fuel rocket. It represented an enormous quantum leap in technology, financed by Nazi Germany in a huge development program that cost at least $ 2 billion in 1944 dollars. 6,084 V-2 missiles were built, 95% of them by 20,000 slave laborers in the last seven months of World War II at a unit price of $ 17,877. As many as 3,225 were launched in combat, primarily against Antwerp and London, and a further 1,000 to 1,750 were fired in tests and training. Despite the scale of this effort, the inaccurate missile did not change the course of the war and proved to be an enormous waste of resources. The British, Americans, and Russians launched a further 86 captured German V-2's in 1945-1952. Personnel and technology from the V-2 program formed the starting point for post-war rocketry development in America, Russia, and France. The A1, A2, A3, and A5 were steps in the development of the missile. Later versions - the A6 through A12 - were planned to take the Third Reich to the planets. |
A-4 German production version. |
Corporal E American short range ballistic missile. Experimental version of Corporal Missile. Nitric acid/Aniline-Furfuyrl alcohol propellants. |
Bumper-WAC German short range ballistic test vehicle. Pioneering US demonstration of a two stage launch vehicle, coupling a V-2 with a WAC Corporal. The first ballistic missile fired from Cape Canaveral. |
R-1A Russian short range ballistic test vehicle. Experimental missile for testing warhead separation. |
Corporal Type 1 American short range ballistic missile. First prototype of Corporal missile. |
R-1V Russian short range ballistic suborbital launch vehicle. The R-1V version was designed for scientific research at altitudes of up to 100 km, including study of cosmic rays; properties of the atmosphere; solar spectra; effects if zero-G and radiation on animals; and development of recovery of the entire missile using parachutes in order to reuse it for further experimental launches. |
R-1B Russian short range ballistic suborbital launch vehicle. The R-1B version was designed for scientific research at altitudes of up to 100 km, including study of cosmic rays; properties of the atmosphere; solar spectra; effects if zero-G and radiation on animals; and development of recovery of the entire missile using parachutes in order to reuse it for further experimental launches. |
Corporal American short range liquid-propellant ballistic missile. The first American operational guided missile, deployed 1954-1964. Replaced by the Sergeant solid-propellant missile. |
Corporal Type 2 American short range ballistic missile. Second prototype of Corporal Missile |
R-1 8A11 Russian short range ballistic missile. Initial production version. |
Redstone Redstone was the first large liquid rocket developed in the US using German V-2 technology. Originally designated Hermes C. Redstones later launched the first US satellite and the first American astronaut into space. |
A-1 (R-1) Soviet designation for a sounding rocket version of the R-1 (Russian-built V-2) used for ionospheric research. |
R-1 Russian short range ballistic missile. Stalin did not decide to proceed with Soviet production of this copy of the German V-2 until 1948. Despite the threatening supervision of the program by Stalin's secret police chief, Beria, and the assistance of German rocket engineers, it took eight years for the German technology to be absorbed and the missile to be put into service. It was almost immediately superseded by later designs, but the effort laid the groundwork for the Soviet rocket industry. Surplus R-1's were converted to use as a sounding rockets for military and scientific research missions. |
R-1D Russian short range ballistic suborbital launch vehicle. The R-1B version was designed for scientific research at altitudes of up to 100 km, including winds aloft, the ionosphere, and effects of spaceflight and recovery of living animals. |
MGM-5A American short range ballistic missile. First production version. |
R-1E Russian short range ballistic suborbital launch vehicle. The R-1E version was designed for scientific research at altitudes of up to 100 km, including winds aloft, air composition, solar radiation, the ionosphere, ozone layer characteristics, and effects of spaceflight and recovery of living animals. |
R-1E (A-1) Russian short range ballistic suborbital launch vehicle. |
MGM-5B American short range ballistic missile. Second production version. |
Sergeant American single-stage solid-propulsion tactical ballistic missile developed for the US Army in 1956-1962. Surplus rockets and the Sergeant's rocket motor (known commercially as Castor) became the basis for many sounding rockets, test vehicles, stages for orbital launch vehicles, and lateral boosters for the Delta space launch vehicle. |
Jupiter C Juno I American short range ballistic missile. Four stage orbital launch version consisting of 1 x Redstone + 1 x Cluster stage 2 + 1 x Cluster stage 3 + 1 x RTV Motor. The fourth stage allowed the Explorer payload to be placed into orbit. |
R-17 Russian short-range ballistic missile. The final refinement of the R-11 design, the R-17, was exported widely and became infamous around the world by its ASCC reporting name - "Scud". It was perhaps the most famous ballistic missile of the post-war period due to its use in the Iran-Iraq 'War of the Cities' and the Gulf War. This was the definitive production version of what was essentially a storable-propellant rocket with the performance of the V-2. The original design was by Makeyev but the missile itself was produced by the Votkinsk Machine Building Plant. |
9M/1/TEMP Russian short range ballistic missile. Two-stage deployed short range missile. Four solid motors strapped together, operating in staged pairs. |
PR-90 Russian short range ballistic missile. Short-range air-augmented ballistic missile. Tested concepts for Gnom ICBM. |
Al Zahar Egyptian short range ballistic missile. United Arab Republic neither confirmed nor denied reports of November 8 that it had successfully launched its first rocket. Dr. Eugen Saenger of the Stuttgart Jet Propulsion Institute in Germany denied any connection with the United Arab Republic program as charged by Israel. |
Al Zafir Egyptian short range ballistic missile. |
MD-620 First Israeli ballistic missile. Developed by Assault in France as the MD-620. Test series included both one and two stage prototypes. Follow-on versions were said to have differed. |
XMGM-52B American short range ballistic missile. |
Pluton French short range ballistic missile. |
MGM-52A American short range ballistic missile. |
MGM-52C American short range ballistic missile. Simplified inertial guided, nuclear or conventional warhead |
I-Scud Russian short-range ballistic missile. |
ATACMS American short range ballistic missile. The ATACMS (Army Tactical Missile System) was the U.S. Army's short/medium-range tactical ballistic missile system from the 1990's. |
Ching Feng Taiwanese short range ballistic missile. |
Prithvi Indian single-stage short range ballistic missile developed from upper stage of Soviet S-75 surface-to-air missile. First units deployed in 1995. Used as an upper stage in the Agni test system. |
Hades French short range ballistic missile. Single stage vehicle |
Iran-130 Iranian short range ballistic missile. |
SSM Korea South Korean short range ballistic missile. |
DF-11 Chinese single-stage solid-propellant short range ballistic missile. Export designation M-11, assembled as Ghaznavi in Pakistan. |
Hwasong 7 North Korean mobile liquid propellant single stage tactical ballistic missile. Derived from Russian R-17, often referred to as 'Scud-D'. The Hwasong had a 700 km range with a 500 kg payload and went into service in 1994. |
Jericho-1 Israeli short range ballistic missile. Follow-on version differed from original French-derived Jericho. Probably used a single 4500 kg solid-propellant motor. |
M-7 Chinese short range ballistic missile. Surface-to-surface derivative of the HQ-2 air defense missile. US designation is CSS-8. Exported to Iran as Tamdar & Tondar in Iran. |
Alacran Argentinian short range ballistic missile. |
Iskander New Russian tactical ballistic missile, conceived as a follow-on to the Scud. First fired on 25 October 1995. |
MB/EE-150 Brazilian short range ballistic missile. |
Condor 1 Argentinian short range ballistic missile. |
MB/EE-350 Brazilian short range ballistic missile. |
Lance American short range ballistic missile, which replaced the Little John, Sergeant and Honest John rockets in US Army service in the 1970's. Retired in 1992. |
Block 1 American short range ballistic missile. In production. Advanced TACtical Missile System, Fire Support , Deep Attack Field Artillery, 1000 bomblets |
Block 1A American short range ballistic missile. In production. |
Block 2 American short range ballistic missile. In development. |
Dhanush Indian short-range, sea-based, liquid-propellant ballistic missile thought to be a variant of the Prithvi. |
ATACMS II American short range ballistic missile. ATACMS Block II is a derivative of the MGM-140 ATACMS (Army Tactical Missile System). The Block II designation applies to ATACMS variants designed to deliver the BAT (Brilliant Anti-Tank) guided submunition. |
Fahd Iraqi short range ballistic missile development based on the Russian S-75 surface-to-air missile. |
LASM Land Attack Standard Missile, a derivative of the Standard Missile SM-2MR naval air-defense designed to provide surface-to-surface fire support for the US Marine Corps. |
Hwasong 5 North Korean mobile liquid propellant single stage tactical ballistic missile. Reverse-engineered from Russian R-17's provided by Egypt around 1980. Often referred to as 'Scud-B'. 340 km range compared to 300 km for the original R-17 design. |
Hwasong 6 North Korean mobile liquid propellant single stage tactical ballistic missile. Derived from Russian R-17, often referred to as 'Scud-C'. The Hwasong had a 500 km range, achieved by halving the payload. |
SS-300 Brazilian short range ballistic missile. |