Tactical ballistic missile
A tactical ballistic missile (TBM), or battlefield range ballistic missile (BRBM), is a ballistic missile designed for short-range battlefield use. Typically, range is less than 1,000 kilometres (620 mi).[1] Tactical ballistic missiles are usually mobile to ensure survivability and quick deployment, as well as carrying a variety of warheads to target enemy facilities, assembly areas, artillery, and other targets behind the front lines. Warheads can include conventional high explosive, chemical, biological, or nuclear warheads. Typically tactical nuclear weapons are limited in their total yield compared to strategic nuclear weapons.
Design
Tactical ballistic missiles fill the gap between conventional rocket artillery and longer-range short-range ballistic missiles. Tactical missiles can carry heavy payloads deep behind enemy lines in comparison to rockets or gun artillery, while having better mobility and less expense than the more strategic theatre missiles. Additionally, due to their mobility, tactical missiles are better suited to responding to developments on the battlefield.
For many nations, tactical missiles represent the upper limit of their land-based military equipment. They can provide a powerful weapon for a very economical price, and in some cases are sought to help level the playing field against opponents who are superior in other areas of military technology. Currently, tactical ballistic missile technology remains within reach for nations that may face difficulties in obtaining other advanced military technologies.
Ballistic missiles are still difficult to defeat on the battlefield. Newer air defense systems have improved ability to intercept tactical missiles, but still can not reliably protect assets against ballistic missile threats. This allows a moderate force of missiles to threaten a superior enemy by penetrating their air defenses better than with conventional aircraft, while providing a deeper strike than conventional artillery.
Propulsion
Early large rockets and missiles were propelled by liquid-propellant rocket engines, as the first types developed. These were replaced as soon as possible by solid fuel rocket motors. Liquid propellants involve cryogenic (liquid oxygen) or corrosive (nitric acid) oxidisers. These must be loaded before launch, delaying the rocket's time into action. This delay was a problem for large strategic missiles, but especially so for tactical.
Missiles, particularly in the Soviet Union, switched to using storable liquid propellants such as IRFNA, inhibited nitric acid. These were still hazardous to handle, but could be stored pre-loaded in the missile. This also allowed the development of single vehicle transporter erector launchers (TEL), rather than the previous convoy of carriers, launchers, fuel vehicles and service vehicles.
Western missiles adopted solid propellants instead,[i] which were inherently storable, and later Warsaw Pact missiles followed suit. Tactical missiles are now almost universally solid-fuelled, except for some states using indigenous derivatives of the original Scud platform.
Specific TBMs
NATO reporting name | Propellant | Range | Introduction | Withdrawal | Origin | Operators | |
---|---|---|---|---|---|---|---|
Al-Samoud 2 | Liquid | 180 km | 2001 | 2003 | Iraq | ||
Al-Hussein | Liquid | 600–650 km | 1987 | 1991 | Iraq | ||
Blue Water | Solid | 1960 (first flight) | cancelled 1962 | United Kingdom | |||
MGM-140 ATACMS | Solid | 300 km | 1986 | 2007 (program terminated, missile remains in service) | United States | ||
MGM-52 Lance | Liquid | 120 km | 1972 | 1992 | United States | ||
PGM-11 Redstone | Liquid | 92.5 km-323 km | 1958 | 1964 | USA | ||
Precision Strike Missile | >500 km | 2023 | USA | ||||
MGM-18 Lacrosse | 19 km | 1959 | 1964 | USA | |||
WS-1 | 60–180 km | ≈1990 | China | ||||
WS-2 / WS-3 | 70–200 km | ≈2004 | China | ||||
DTI-1 | 60–180 km | Thailand | |||||
Hrim-2 | 280–500 km | Ukraine | |||||
Shaurya | Two-stage solid | 700-1900 km | 2011 | India | |||
Prahaar | Solid | 150 km | 2011 | India | |||
Pragati | Solid | 170 km | 2013 | India | |||
Pranash | Solid | 200 km | TBD | ||||
Pralay | Solid | 150-500 km | TBD | India | |||
Ghaznavi (missile) | Solid | 290–320 km | 2004 | Pakistan | |||
Nasr/Hatf IX | Solid | 70 km | 2013 | Pakistan | |||
Abdali/Hatf-II | Solid | 180 km | 2002 | Pakistan | |||
Hatf-I | Solid | 70 km | 1990 | Pakistan | |||
Hatf-1A | Solid | 100 km | 1990 | Pakistan | |||
Hatf-1B | Solid | 100 km | 1990 | Pakistan | |||
Sky Spear | Solid | 120–300 km | 2001 | Taiwan | |||
J-600T Yıldırım | Solid | 150–900 km | 1998 | Turkey | |||
TOROS | Solid | 100–160 km | Turkey | ||||
Bora | Solid | 280–700 km | 2017 | Turkey | |||
T-300 Kasırga | 100–120 km | Turkey | |||||
R-11 Zemlya | SS-1b Scud-A | Liquid | 180 km | 1958 | Soviet Union | ||
2K1 Mars | FROG-2 | Solid | 7–18 km | Soviet Union | |||
R-17/R-300 Elbrus | SS-1c Scud-B SS-1d Scud-C SS-1e Scud-D | Liquid | 300–700 km | 1964 | Soviet Union | ||
OTR-21 Tochka | SS-21 Scarab | Solid | 70–185 km | 1975 | Soviet Union | ||
OTR-23 Oka | SS-23 Spider | Solid | 500 km | 1979 | 1987 | Soviet Union | |
2K6 Luna | Frog-3, Frog-5 | 10–50 km | 1960 | 1982 | Soviet Union | ||
9K52 Luna-M | Frog-7 | 70 km | 1964 | Soviet Union | |||
LORA | 400–800 km | 2005 | Israel | Azerbaijan | |||
Hwasong-11 (KN-02) | Solid | 120–160 km | 2008 | North Korea | Syria | ||
Hwasong-11A (KN-23) | Solid | 450 km[2] | 2018 | North Korea | |||
Hwasong-11B (KN-24) | Solid | 410 km[3] | 2019 | North Korea | |||
Hwasong-11D | Solid | 100–300 km | 2022 | North Korea | |||
KN-25 | 380 km | 2019 | North Korea | ||||
9K720 Iskander | SS-26 Stone | Solid | 400–500 km | 2006 | Russia | ||
Predator Hawk | 300–400km | 2016 | Israel | Morocco | |||
Hyunmoo-1 | Solid | 180 km | 1977 | South Korea | |||
Hyunmoo-2A | Solid | 300 km | 2006 | South Korea | |||
Ure-1 | Solid | 180 km | 2022 | South Korea | |||
BRE8 King Dragon/Fire Dragon | Solid | 280–300 km | 2014? | China | |||
Burkan-1 | 800 km | 2016 | Yemen | ||||
al-Najm al-Thaqib-1 | 45 km | 2015 | Yemen | ||||
al-Najm al-Thaqib-2 | 75 km | 2015 | Yemen | ||||
Fajr-5 | Solid | 180 km | 1990s | Iran | |||
Shahab-1 | 350 km | 1987 | ~2016 | Iran | Syria | ||
Shahab-2 | Liquid | 500 km | 1990 | 2016 | Iran | Syria | |
Fateh-110 | Solid | 300 km | 2002 | Iran | |||
Fateh-313 | Solid | 500 km | 2015 | Iran | Syria | ||
Qiam 1 | Liquid | 800 km | 2010 | Iran | Yemen | ||
Zelzal-1 | Solid | 160 km | 1990 | Iran | Syria | ||
Zelzal-2 | Solid | 210 km | 1998 | Iran | |||
Zelzal-3 | Solid | 200–250 km | 2007 | Iran | Syria | ||
Naze'at 6-H | Solid | 80–100 km | 1980's | Iran | |||
Naze'at 10-H | Solid | 100–130 km | 1980's | Iran | |||
Jerina-1 | Solid[4] | 285-300 km | 2017 | ||||
Jerina-2 | Liquid | 75 km | 2017 |
See also
Notes
- ^ The liquid-fuelled MGM-52 Lance was one exception, remaining in service until the end of the Cold War.
References
- ^ Davenpot, Kesley. "Worldwide Ballistic Missile Inventories". Arms Control Association. Retrieved 21 May 2025.
- ^ "KN-23". Missile Threat. Retrieved 12 March 2021.
- ^ "KN-24". Missile Threat. Retrieved 12 March 2021.
- ^ "EDePro, Engine Development and Production".