fbpx
Wikipedia

AGM-78 Standard ARM

The AGM-78 Standard ARM was an anti-radiation missile developed by General Dynamics, United States. It was built on the airframe of the RIM-66 Standard surface-to-air missile, resulting in a very large weapon with considerable range, allowing it to attack targets as much as 50 miles (80 km) away.

AGM-78 Standard ARM
TypeAir-to-surface anti-radiation missile
Place of originUnited States
Service history
In service1968–1988
WarsVietnam War
Production history
Designed1967
Produced1967–1976
No. built3,000+
Specifications
Mass620 kg (1370 lb)
Length4.57 m (15 ft)
Diameter34.3 cm (13.5 in)
Wingspan108 cm (42.5 in)
Warhead weight97 kg (215 lb) blast-fragmentation

EngineAerojet MK 27 MOD 4 dual-thrust solid-fueled rocket
Operational
range
90 km (56 mi)
Maximum speed Mach 1.8
Guidance
system
Passive radar homing
Launch
platform
A-6B/E Intruder, F-105G Thunderchief, F-4G Phantom II

Overview edit

Originally developed for the US Navy during the late 1960s, the AGM-78 was created in large part because of the limitations of the AGM-45 Shrike, which suffered from a small warhead, limited range and a poor guidance system. General Dynamics was asked to create an air-launched ARM by modifying the RIM-66 SM-1 surface-to-air missile. This use of an "off the shelf" design greatly reduced development costs, and trials of the new weapon began in 1967 after only a year of development. The first operational missiles were issued in early 1968.

The AGM-78 was nicknamed the "Starm", an abbreviation of Standard ARM.[citation needed] The first version of the missile, the A1 Mod 0, was little more than an air-launched RIM-66 with the Shrike's anti radar seeker head attached to the front. An Aerojet Mark 27 MOD 4 dual-thrust solid-rocket-powered the missile, which was fitted with a blast-fragmentation warhead. Although more capable, the AGM-78 was much more expensive than the AGM-45 Shrike which continued in service for some time. The new missile was carried by the F-105F/G and the A-6B/E.

Variants edit

 
A 6010th WWS F-105G taking off to North Vietnam, 1971.
 
Israeli Keres AGM-78 Standard ARM launcher at IAF Museum

An inert training version of the AGM-78A was built as ATM-78A. Of equal size, mass and shape, the missile lacked a seeker head, warhead, or propulsion systems and was essentially just a dead weight.

An A2 model introduced a bomb damage assessment (BDA) capability and an SDU-6/B phosphorus target marker flare to facilitate targeting of the site for follow-up attacks.

In 1969 an improved model called the AGM-78B was produced. This featured a broadband seeker which allowed the missile to be used against a much wider variety of targets without having to select the seeker before the mission. A simple memory circuit was also included, allowing the missile to attack a target once it locked on, even if the radar was shut down. Previous ARMs would veer off course and miss when they lost a target, and as a result flipping the radar on and off had become a standard tactic for missile batteries.

Some early AGM-78A1s were updated with the new memory circuit and seeker. These missiles were designated as the AGM-78A4. The AGM-78B was the most important version of the missile, and was widely used by the Air Force's F-4G Phantom II Wild Weasel aircraft.

A training version of the AGM-78B was created, and was known as the ATM-78B.

In the early 1970s the AGM-78C was produced. A US Air Force project, the C model was primarily intended to be more reliable and cheaper to build. It had a SDU-29/B white phosphorus target marker. Some older missiles were upgraded to the AGM-78C standard. As before, an ATM-78C training missile was produced.

Between 1973 and 1976 the AGM-78D was produced, introducing a new motor. A follow-up missile, the AGM-78D2, had an active optical fuze, still greater reliability, and a new 100 kg (220 lb) blast-fragmentation warhead. The ATM-78D training missile followed.

The RGM-66D shipborne anti-radiation missile used the basic AGM-78 airframe along with features of the RIM-66 and AIM-97 Seekbat air-to-air missile.

Including all versions, over 3,000 AGM-78 missiles were built. Production stopped in the late 1970s, but the missile continued in service for almost a decade before the last examples were replaced by the AGM-88 HARM in the late 1980s.

 
Map with operators of the AGM-78 Standard ARM in blue

Operators edit

External links edit

  • Designation-systems.net

standard, also, standard, missile, anti, radiation, missile, developed, general, dynamics, united, states, built, airframe, standard, surface, missile, resulting, very, large, weapon, with, considerable, range, allowing, attack, targets, much, miles, away, typ. See also Standard Missile The AGM 78 Standard ARM was an anti radiation missile developed by General Dynamics United States It was built on the airframe of the RIM 66 Standard surface to air missile resulting in a very large weapon with considerable range allowing it to attack targets as much as 50 miles 80 km away AGM 78 Standard ARMTypeAir to surface anti radiation missilePlace of originUnited StatesService historyIn service1968 1988WarsVietnam WarProduction historyDesigned1967Produced1967 1976No built3 000 SpecificationsMass620 kg 1370 lb Length4 57 m 15 ft Diameter34 3 cm 13 5 in Wingspan108 cm 42 5 in Warhead weight97 kg 215 lb blast fragmentationEngineAerojet MK 27 MOD 4 dual thrust solid fueled rocketOperationalrange90 km 56 mi Maximum speedMach 1 8GuidancesystemPassive radar homingLaunchplatformA 6B E Intruder F 105G Thunderchief F 4G Phantom II Contents 1 Overview 2 Variants 3 Operators 4 External linksOverview editOriginally developed for the US Navy during the late 1960s the AGM 78 was created in large part because of the limitations of the AGM 45 Shrike which suffered from a small warhead limited range and a poor guidance system General Dynamics was asked to create an air launched ARM by modifying the RIM 66 SM 1 surface to air missile This use of an off the shelf design greatly reduced development costs and trials of the new weapon began in 1967 after only a year of development The first operational missiles were issued in early 1968 The AGM 78 was nicknamed the Starm an abbreviation of Standard ARM citation needed The first version of the missile the A1 Mod 0 was little more than an air launched RIM 66 with the Shrike s anti radar seeker head attached to the front An Aerojet Mark 27 MOD 4 dual thrust solid rocket powered the missile which was fitted with a blast fragmentation warhead Although more capable the AGM 78 was much more expensive than the AGM 45 Shrike which continued in service for some time The new missile was carried by the F 105F G and the A 6B E Variants edit nbsp A 6010th WWS F 105G taking off to North Vietnam 1971 nbsp Israeli Keres AGM 78 Standard ARM launcher at IAF Museum An inert training version of the AGM 78A was built as ATM 78A Of equal size mass and shape the missile lacked a seeker head warhead or propulsion systems and was essentially just a dead weight An A2 model introduced a bomb damage assessment BDA capability and an SDU 6 B phosphorus target marker flare to facilitate targeting of the site for follow up attacks In 1969 an improved model called the AGM 78B was produced This featured a broadband seeker which allowed the missile to be used against a much wider variety of targets without having to select the seeker before the mission A simple memory circuit was also included allowing the missile to attack a target once it locked on even if the radar was shut down Previous ARMs would veer off course and miss when they lost a target and as a result flipping the radar on and off had become a standard tactic for missile batteries Some early AGM 78A1s were updated with the new memory circuit and seeker These missiles were designated as the AGM 78A4 The AGM 78B was the most important version of the missile and was widely used by the Air Force s F 4G Phantom II Wild Weasel aircraft A training version of the AGM 78B was created and was known as the ATM 78B In the early 1970s the AGM 78C was produced A US Air Force project the C model was primarily intended to be more reliable and cheaper to build It had a SDU 29 B white phosphorus target marker Some older missiles were upgraded to the AGM 78C standard As before an ATM 78C training missile was produced Between 1973 and 1976 the AGM 78D was produced introducing a new motor A follow up missile the AGM 78D2 had an active optical fuze still greater reliability and a new 100 kg 220 lb blast fragmentation warhead The ATM 78D training missile followed The RGM 66D shipborne anti radiation missile used the basic AGM 78 airframe along with features of the RIM 66 and AIM 97 Seekbat air to air missile Including all versions over 3 000 AGM 78 missiles were built Production stopped in the late 1970s but the missile continued in service for almost a decade before the last examples were replaced by the AGM 88 HARM in the late 1980s nbsp Map with operators of the AGM 78 Standard ARM in blueOperators edit nbsp United States nbsp Israel nbsp IranExternal links edit nbsp Wikimedia Commons has media related to AGM 78 Standard ARM USAF Museum AGM 78 factsheet Designation systems net Retrieved from https en wikipedia org w index php title AGM 78 Standard ARM amp oldid 1168092049, wikipedia, wiki, book, books, library,

article

, read, download, free, free download, mp3, video, mp4, 3gp, jpg, jpeg, gif, png, picture, music, song, movie, book, game, games.