| SIDEWINDER air-to-air (AIM-9M) Missile: | |
| Dimensions | Length: 9' 5"; Diameter: 5" |
| Wing Span | 2' 1" |
| Weight | 195 pounds |
| Speed | More than 1,900 mph |
| Range | More than 3.5. nautical miles |
| Propulsion | Single-stage, solid propellant reduced smoke motor |
| Warhead | Annular blast fragmentation; weight: 25 pounds |
| Builder(s) | |
| Notes |
The Sidewinder air-to-air missile is a short-range,
dogfight missile used by all Navy fighters and attack aircraft
against hostile aircraft. Sidewinder is one of the oldest, least expensive and most successful missiles in the entire U.S. weapons inventory. The prototype of this heat-seeking missile first was fired more than 30 years ago; since then various versions of it have been produced for more than 27 nations. The latest version, AIM-9M, was introduced in 1982, has a significantly improved infrared counter-measure capability. |
| SPARROW air-to-air/surface-to-air (AIM/RIM-7M) Missile: | |
| Dimensions | Length: 12'; Diameter: 8" |
| Wing Span | 3' 4" |
| Weight | 510 pounds |
| Speed | More than 2,660 mph |
| Range | More than 30 nautical miles |
| Propulsion | Solid propellant rocket motor |
| Warhead | Blast Fragment, high explosive |
| Notes |
The much improved AIM/RIM-74 version of this highly
successful air-to-air and surface-to-air missile has considerably
greater invulnerability to electronic counter measures (ECM),
better target tracking capability, and a new low altitude active
fuse. It is the fifth operational missile of the Sparrow family and
can be employed against attacking aircraft at all tactical speeds
and altitudes in all weather. The RIM-7M, with folding wings and clipped tail fins, is compatible with the NATO Sea Sparrow launcher. This latest version of the Sparrow family entered the Navy's inventory in 1983. It continues to be one of the most heavily procured missiles. See AMRAAM. |
| PHOENIX air-to-air (AIM-54C) Missile: | |
| Dimensions | Length: 13'; Diameter: 15" |
| Wing Span | 3' |
| Weight | 1,024 pounds |
| Speed | In excess of 3,040 mph |
| Range | In excess of 104 nautical miles |
| Propulsion | Solid propellant rocket motor |
| Warhead | Proximity fuse, high explosive |
| Builder(s) | |
| Notes |
The Phoenix missile was introduced into the fleet with
the F-14A aircraft and AN/AWG-9 weapons control system in 1974. The
AN/AWG-9 is capable of long range tracking of multiple hostile air
targets and to launch up to six missiles against six targets
simultaneously. The missile has great range and intercept
capability against high speed maneuvering targets at both high and
low altitude. The current version, AIM-54C, now in production, has significantly improved the capability for counter-countermeasures. |
| HARM air-to-surface (AGM-88A) Missile: | |
| Dimensions | Length: 13' 8"; Diameter: 10" |
| Wing Span | 3' 8" |
| Weight | 807 pounds |
| Speed | More than 760mph |
| Range | 50 plus nautical miles |
| Propulsion | Two-stage solid propellant rocket motor |
| Warhead | Blast fragmentation |
| Builder(s) | Texas Instruments |
| Notes |
This Air-to-surface missile was designed to destroy or suppress
enemy electronic emitters, especially those associated with radar
sites used to direct anti-aircraft guns and surface-to-air missiles. Harm is a high-speed anti-radiation missile which succeeds Shrike and Arm as the Navy's primary anti-radiation, defense-suppression air-to-surface missile. It proved effective against Libyan targets in the Gulf of Sidra in 1986. FY 1988 cost for 766 Harm missiles is $194.7 million; FY 1989 cost for 1766 missiles is $404.9 million. |
| AMRAAM air-to-air (AIM-120A) Missile: | |
| Dimensions | Length: 12'; Diameter: 7" |
| Wing Span | 1' 9" |
| Weight | 335 pounds |
| Speed | More than 760 mph |
| Range | Greater than 35 nautical miles (depending on launch/target parameters) |
| Propulsion | Directed rocket motor |
| Warhead | Blast high explosive |
| Builder(s) | Hughes Aircraft/Raytheon Co. |
| Notes |
The AIM-120A, Advanced Medium Range Air-to-Air Missile (AMRAAM) is the next generation
all-weather, radar guided, beyond visual range missile designed to
provide launch and leave capability and multiple target engagement capability. The AMRAAM missile is the follow-on to the Sparrow missile and will be deployed on F-14D and F/A-18 C/D A/C. It's faster, smaller, lighter and better able to attack at a lower level than the Sparrow. The pilot will be able to aim and fire several missiles at multiple targets simultaneously. The Navy has requested procurement of 150 AMRAAM missiles in FY 1990 at a cost of approximately $129 million. Raytheon has been certified as a second production source. |
| TACIT RAINBOW (AGM-136A) Missile: | |
| Dimensions | Length: 8' 4"; Diameter: 19" |
| Wing Span | 5' 1.5" |
| Weight | 430 pounds |
| Speed | 250+ mph |
| Range | 90+ nautical miles |
| Propulsion | Turbo-Jet Engine |
| Builder(s) | Northrop, Ventura Unit |
| Notes |
Air-to-surface missile designed to provide persistent air defense
suppression capability to cost effectively counter -- in
conjunction with HARM and other defense suppression systems --
hostile integrated air defense systems. Tacit Rainbow is a long range standoff, loitering anti-radiation homing missile capable of launch from a wide variety of tactical aircraft. Production will start in Fiscal Year 1992. |
| IR MAVERICK (AGM-65F) Missile: | |
| Dimensions | Length: 8' 2"; Diameter: 12" |
| Wing Span | 2' 4.5" |
| Weight | 300 pounds |
| Speed | Supersonic, boost/sustain |
| Range | 6-12 nautical miles |
| Propulsion | Two-stage solid propellant rocket motor |
| Warhead | Penetrating/Blast |
| Builder(s) | Hughes and Raytheon |
| Notes |
Air-to-surface missile designed for day/night war-at-sea and land
interdiction against small ships and bunkers. IR Maverick is a forward-fired, infrared guided weapon. It is a modified version of the U.S. Air Force TV Maverick with a larger improved warhead, out of line igniter, and IR guidance section optimized for ship tracking. IR Maverick is planned for employment by the Navy/U.S. Marine Corps on the AV-8B, F/A-18 and A-6E SWIP aircraft. |
| BIGEYE Chemical Weapon (BLU-80/B): | |
| Dimensions | Length: 7' 6"; Diameter: 13.25" |
| Wing Span | 1' 5.25" |
| Weight | 595 pounds |
| Warhead | VX Agent Weight: 180 pounds |
| Builder(s) | The Marquardt Company |
| Notes |
Air-to-ground retaliatory chemical weapon designed to
deter adversaries from using their chemical weapons. Bigeye is a tri-service, safe-to-handle binary chemical weapon. When employed, Bigeye is designed to delay and disrupt airfields, troops and logistical lifelines by forcing an enemy into a chemical protective posture. The Bigeye metal parts contract was awarded in June 1988 for the procurement of production-representative operational test units, trainers and Safe Separation Test Vehicles. |
| Advanced Rocket System: | |
| Propulsion | Current MK 66 and/or high performance |
| Warhead | Color marking; anti-personnel, material, armor, helicopter and coastal shipping chaff; flare; smoke screening; night marking; and training |
| Notes |
Provide a high volume of air-to-ground fire from
stand-off ranges against a broad target spectrum. The Advanced Rocket System plans to "neckdown" the 2.75-Inch and 5-Inch Rocket Systems to one that meets the requirements of the Anti-Surface Warfare Master Plan. The current program will maximize available RDT&E funds through the use of currently ongoing or planned Product Improvement Programs, NDI and FWE/NCT candidate components. The motor will have a minimum effective range of 10,000 meters direct fire and 15,000 meters loft delivery is required. |
| The Advanced Interdiction Weapon System (AIWS): | |
| Dimensions | Length: NTE 168" Width: NTE 24" Height: NTE 21" |
| Weight | NTE 1,965 pounds |
| Notes |
Low cost air-to-ground weapon to attack less than high
value targets day or night with capability for stand-off outside
close in defense. The Advanced Interdiction Weapon System (AIWS) entered the Demonstration and Validation Phase during the third quarter of FY-89. A key element in the Strike Anti-Surface Warfare Master Plan, the AIWS will replace Skipper/Laser Guided Bombs, Walleye and Laser Maverick beginning in the mid-1990's. The first variant will be inertially guided and have a cluster warhead for use against area targets outside of close-in-defenses. Later variants will include a terminal seeker, GPS Receiver, Man-in-the-Loop capability and unitary warhead for use against individual targets outside of Point Defenses. The AIWS will be employed from the F/A-18, A-6, A-12 and AV-8B aircraft. |
| Advanced Bomb Family (ABF): | |
| Warhead | 500 pound/1,000 pound (insensitive high explosive fill) |
| Fuzing | Integral unit; highly integrated, multi-function, electronic device with provisions for plug-in special mission kits |
| Fin Assembly | Stabilizer/retarder (high/low drag options) |
| Aircraft Interface | Single MIL-STD-1760 connection |
| Notes |
Provide two affordable All-UpRound (AUR) weapons to meet
the general purpose bombing requirements for increased blast,
fragmentation, and penetration effects against a broad target
spectrum. The Advanced Bomb Family (ABF) will replace the MK-80 series bomb components with two versatile weapons: a 500 pound class bomb optimized for blast and fragmentation, and a 1,000 pound class bomb with improved penetration capabilities. These weapons will make maximum use of common components and modern technology to improve safety, logistics, and tactical flexibility while decreasing life cycle costs. The ABF will satisfy all insensitive munitions requirements. The bombs will be compatible with current and future tactical aircraft. |
| PHALANX Close-In Weapons System (CIWS MK-15): | |
| Weight | 12,500 pounds |
| Gun | M61A1 Vulcan (gatling-type) |
| Ammunition | 20mm with high density penetrating projectile |
| Magazine Capacity | 989 rounds |
| Firing Rate | 3,000 rounds per minute |
| Builder(s) | General Dynamics' Pomona Division |
| Notes |
The Phalanx Close-In Weapons System (CIWS) is a
last-ditch defense against anti-ship missiles. It combines a single
mount fire-control radar and a six-barrel Gatling gun firing
depleted-uranium projectiles at a rate of 3,000 rounds per minute.
Its projectiles are 2.5 times heavier than those made of steel.
A total, fully integrated weapons system, it automatically carries
out search, detection, automatic threat evaluation, tracking, and
firing. Its reliability has been increasing constantly. The Navy
plans ultimately to install 626 systems aboard ships of the fleet;
and has ensured every Phalanx selected ship scheduled for
deployment to the Middle East receives its system prior to
deployment. The Navy also is modifying over 400 of its CIWS installations to improve their capability and enhanced operability, maintainability and reliability. Competitive procurement commenced in 1988. |
| TOMAHAWK Cruise Missile (BGM-109): | |
| Dimensions | Length: 18' 3"; with booster, 20' 6" Diameter: 20.4" |
| Wing Span | 8' 9" |
| Weight | 2,650 pounds; 3,200 pounds with booster |
| Speed | Subsonic - about 550 mph |
| Range | Land attack, nuclear warhead: 1,350 nautical land attack, conventional warhead: 600 nautical miles anti-ship configuration: over 250 nautical miles |
| Propulsion | Williams International F107-W-R-400 cruise turbo-fan engine; solid-fuel booster |
| Warhead | Conventional: 1,000 pounds - W-80 submunitions dispenser with combined effect bomblets bullpup: Nuclear |
| Builder(s) | General Dynamics, Convair Division McDonnell Douglas |
| Notes |
Tomahawk is an all-weather submarine/surface combatant
launched anti-ship or land attack cruise missile. After launch, a
solid propellant rocket booster propels the missile until a small
turbofan engine takes over for the cruise portion of the flight.
The land attack version of Tomahawk has an inertial and terrain
contour matching (TERCOM) guidance. TERCOM uses a stored map
reference to compare with the actual terrain. This determines the
missile's position. If necessary, a course correction is then made
to place the missile on course to the target. The anti-ship version
has a modified Harpoon cruise missile guidance system. This permits
Tomahawk to be launched and fly at low altitudes in the general
direction of an enemy warship to avoid radar detection. At a
programmed distance, the missile begins an active radar search to
seek out, acquire and hit the target ship. Tomahawk is a highly survivable weapon against predicted hostile defense systems. Radar detection is difficult because the missile has a very small cross-section and can fly at extremely low altitudes. Similarly, infrared detection is difficult because the turbofan engine emits a low level of heat. The anti-ship variant of Tomahawk uses a combined active radar seeker and passive system to seek out, engage and destroy a hostile ship at long range. The Tomahawk weapon system is dual-sourced and is built by both General Dynamics/Convair and McDonnell Douglas Astronautics Companies. |
| HARPOON Cruise Missile (R/U/AGM-84): | |
| Dimensions | Length: 15' (surface/submarine launched) Length: 12' 7" (air launched) Diameter: Missile Body - 1' 2" |
| Wing Span | 3' with booster fins and wings |
| Propulsion | Turbojet and solid propellant booster for surface/submarine launch |
| Warhead | 500 pounds, high explosive, blast penetrator |
| Builder(s) | McDonnell Douglas |
| Notes |
MISSION: Destroy hostile surface targets such as combatants,
submarines or other shipping. Harpoon is a medium range, rocket boosted, turbo sustained, anti-ship cruise missile capable of being launched from surface ships, submarines or (without the booster) from aircraft. It was introduced in the fleet on ships and submarines in 1977, and on the P-3 series aircraft in 1979. Day-night and all-weather, the Harpoon is being improved to add range and to decrease altitude in its sea-skimming mode. The Harpoon was used effectively in attacks on Libyan targets in the Gulf of Sidra in 1986. The Navy is now developing a new infrared Harpoon variant called SLAM (Standoff Land Attack Missile). In FY 1987, the Navy bought 82 Harpoon missiles at a cost of $688,594 each; FY 1988, 83 missiles at $752,600 each; and FY 1989, 47 missiles at $886,947 each. |
| POLARIS Missile: | |
| POSEIDON (C-3) Missile: | |
| Dimensions | Length: 34 feet; Diameter: 74 inches |
| Weight | 65,000 pounds |
| Range | 2,500 nautical miles |
| Propulsion | Two-stage, solid-fuel rocket with inertial guidance |
| Warhead | Thermonuclear MIRV - (Multiple Independently Targeted Re-entry Vehicle) |
| Builder(s) | Lockheed Missiles and Space Co., Inc., Sunnyvale, CA |
| TRIDENT I (C-4) Missile: | |
| Dimensions | Length: 34 feet; Diameter: 74 inches |
| Weight | 73,000 pounds |
| Range | 4,000 nautical miles |
| Propulsion | Three-stage soild-fuel rocket, with inertial guidance |
| Warhead | Thermonuclear MIRV - (Multiple Independtly Targeted Re-entry Vehicle) and (Maneuverable Re-entry Vehicle) |
| Builder(s) | Lockheed Missiles and Space Co., Inc., Sunnyvale, CA |
| Notes |
Trident I (C-4) was first deployed in 1979 and will
remain on patrol until phased out in the late 1990s. This missile
was designed to the same dimensions as the Poseidon missile which
allows it to be carried in existing Posidon submarines, as well as
the new Trident submarines. The Trident system makes possible deployment of an improved missile carrying submarine, the Ohio class, with a much longer range strategic ballistic missile, offsetting improvements in Soviet anti-submarine warfare capability by vastly increasing the area in which submarines can operate and still have their missiles reach their target. Trident I has a range almost double that of the Poseidon missile it replaces. It will be deployed in the first eight submarines of the Ohio class and in 12 of the remaining 31 Layfayette class fleet ballistic missile submarines remaining in the fleet. |
| Trident II (D-5) Missile: | |
| Dimensions | Length: 44 feet; Diameter: 83 inches |
| Weight | 130,000 pounds (approximate) |
| Range | Greater than 4,000 nautical miles |
| Propulsion | Three-stage solid-propellant rocket, with inertial guidance |
| Warhead | Thermonuclear MIRV - (Multiple Independently Targetable Re-entry Vehicle) (Maneuverable Re-entry Vehicle) |
| Builder(s) | Lockheed Missiles and Space Co., Inc., Sunnyvale, CA |
| Notes |
The Trident II (D-5) is the sixth generation member of
the U.S. Navy's Fleet Ballistic Missile (FBM) program that started
in 1956. Since then the Polaris (A1), Polaris (A2), Polaris (A3),
Poseidon (C3), and Trident I (C4) have served as a significant
deterrent to nuclear aggression. At present the U.S. Navy deploys
Poseidon (C3) and Trident I (C4), having retired the Polaris family
of missiles. The first deployment of Trident II will occur in late
1989 aboard the USS Tennessee (SSBN 734). The Trident II (D-5) is a three stage, solid propellant inertially guided FBM with a range of more than 4,000 nautical miles (4,600 statute miles). A considerable increase and payload was incorporated into Trident II by encasing the first two stages in epoxied graphite, and the third-stage in the filament-wound Kevlar. Also for increasing the missile's range is the aerospike, a telescoping outward extension that reduces frontal drag by about 50 percent. The new Trident/Ohio class submarines will each carry 24 Trident II missiles that can be launched under water or on the surface. Trident II is ejected by the pressure of expanding gas within the launch tube upon firing. When the missile attains sufficient distance from the submarine, the first stage motor ignites, the aerospike extends, and the boost stage begins. After about 65 seconds the first-stage motor and interstage separate from the missile, allowing the second-stage motor to ignite and continue boost phase for approximately 65 seconds. With separation, the third-stage burns for nearly 40 seconds, concluding the boost phase. At this point the missile is travelling in excess of 20,000 feet per second; the post-boost control system provides thrust and control to the equipment section until all re-entry bodies have been deployed. Periodic test launches with dummy warheads ensure high system reliability. |
| 16inch/45-cal Mark/Model: I | |
| Gun Weight | 103 tons |
| A.P. Shot Weight | 2461 pounds
muzzle velocity: 2953 fps Charge Weight: 640 pounds |
| Builder(s) | British Naval Ordnance |
| 16inch/50-cal Mark/Model: II | |
| Gun Weight | 128 tons |
| A.P. Shot Weight | 2100 pounds
muzzle velocity: 2800 fps |
| Builder(s) | Washington Gun Factory |
| 16inch/45-cal Mark/Model: I | |
| Gun Weight | 105 tons |
| A.P. Shot Weight | 2100 pounds
muzzle velocity: 2600 fps |
| Builder(s) | Washington Gun Factory |
| 15inch/42-cal Mark/Model: I | |
| Gun Weight | 97 tons |
| A.P. Shot Weight | 1920 pounds
muzzle velocity: 2450 fps Charge Weight: 640 pounds |
| Builder(s) | British Naval Ordnance |
| 14inch/50-cal Mark/Model: IV | |
| Gun Weight | 81 tons |
| A.P. Shot Weight | 1400 pounds
muzzle velocity: 2800 fps |
| Builder(s) | Washington Gun Factory |
| 14inch/45-cal Mark/Model: I | |
| Gun Weight | 63.3 tons |
| A.P. Shot Weight | 1400 pounds
muzzle velocity: 2600 fps max. penetration firing capped A.P. directly against K.C. armor @ 9000 yds.: 18" |
| Builder(s) | Washington Gun Factory |
| 12inch | |
| Gun Weight | |
| A.P. Shot Weight |
muzzle velocity: |
| Builder(s) | Washington Gun Factory |
| 8inch Mark/Model: 71 | |
| A.P. Shot Weight | 200 pounds |
| 8inch/55-cal Mark/Model: IX | |
| Gun Weight | 19.7 tons |
| A.P. Shot Weight | 250 pounds
muzzle velocity: 3000 fps |
| Builder(s) | Washington Gun Factory |
| 6inch/53-cal Mark/Model: XII | |
| Gun Weight | 10 tons |
| A.P. Shot Weight | 105 pounds
muzzle velocity: 3000 fps |
| Builder(s) | Washington Gun Factory |
| 6inch/47-cal | |
| Gun Weight | |
| A.P. Shot Weight |
muzzle velocity: |
| Builder(s) | Washington Gun Factory |
| 5inch/54-Caliber Lightweight Gun (MK 42): | |
| 5inch/54-Caliber Lightweight Gun (MK 45): | |
| Notes | Deliveries began in 1971 and will continue through the 1990s for CG-47 and the DDG-51 ship classes. |
| 5inch/51-cal Mark/Model: VII | |
| Gun Weight | 5 tons |
| A.P. Shot Weight | 50 pounds
muzzle velocity: 3150 fps max. penetration firing capped A.P. directly against K.C. armor @ 3000 yds.: 3.4" |
| Builder(s) | Washington Gun Factory |
| 5inch/38-cal (DP) | |
| Builder(s) | Washington Gun Factory |
| 5inch/25-cal (AA) | |
| Builder(s) | Washington Gun Factory |
| 4inch/50-cal Mark/Model: IX | |
| Gun Weight | 3.0 tons |
| A.P. Shot Weight | 33 pounds
muzzle velocity: 2900 fps |
| Builder(s) | Washington Gun Factory |
| 4inch/50-cal Mark/Model: VIII | |
| Gun Weight | 2.9 tons |
| A.P. Shot Weight | 33 pounds
muzzle velocity: 2800 fps max. penetration firing capped A.P. directly against K.C. armor @ 3000 yds.: 2.6" |
| Builder(s) | Washington Gun Factory |
| 4inch/50-cal Mark/Model: VII | |
| Gun Weight | 2.6 tons |
| A.P. Shot Weight | 33 pounds
muzzle velocity: 2500 fps max. penetration firing capped A.P. directly against K.C. armor @ 3000 yds.: 2.2" |
| Builder(s) | Washington Gun Factory |
| 4inch/40-cal Mark/Model: III, IV, V, VI | |
| Gun Weight | 1.5 tons |
| A.P. Shot Weight | 33 pounds
muzzle velocity: 2000 fps max. penetration firing capped A.P. directly against K.C. armor @ 3000 yds.: 1.7" |
| Builder(s) | Washington Gun Factory |
| 3inch/50-cal Mark/Model: X | |
| Gun Weight | 1.15 tons |
| A.P. Shot Weight | 13 pounds
muzzle velocity: 2700 fps |
| Builder(s) | Washington Gun Factory |
| 3inch/50-cal Mark/Model: V, VI, S-A | |
| Gun Weight | 1.0 tons |
| A.P. Shot Weight | 13 pounds
muzzle velocity: 2700 fps max. penetration firing capped A.P. directly against K.C. armor @ 3000 yds.: 1.2" |
| Builder(s) | Washington Gun Factory |
| 3inch/50-cal Mark/Model: II, III | |
| Gun Weight | .9 tons |
| A.P. Shot Weight | 13 pounds
muzzle velocity: 2700 fps max. penetration firing capped A.P. directly against K.C. armor @ 3000 yds.: 1.2" |
| Builder(s) | Washington Gun Factory |
| 76MM/62-Caliber Lightweight Gun (MK 75): | |
| Builder(s) | OTO Melara of La Spezia, Italy |
| Notes | Approved for service use in September 1975. |
| 3 pounder | |
| Notes | 1.85" diam. projectile. |
| 5 pounder | |
| 6 pounder | |
| Notes | 2.244" diam. projectile. |
| 40mm | |
| 20mm | |
| 40mm Gun System: | |
| Gun | Bofors 40mm |
| Ammunition | 40mm |
| Magazine Capacity | hopper capacity: 6 rounds; 4 rounds/"clip"; 4 clips/ammo can. |
| Firing Rate | 40 - 60 rpm |
| Loading Mechanism | manual |
| Cooling | air/water |
| Mount | open with waist-high splinter shield. |
| Barrel(s) | 1, 2, 4 |
| Gun Crew | 1 barrel: 4 (2 loaders, 1 ptr./trnr, 1 mount capt.) 2 barrel: 7 (4 loaders, 1 pointer, 1 trainer, 1 mount capt.) |
| Fire Control | local/remote |
| Builder(s) | Singer and others |
| Italian Breda 40mm Gun System: | |
| Gun | Bofors 40mm L/70 |
| Ammunition | 40mm |
| Magazine Capacity | 800 rounds |
| Firing Rate | 600 rpm |
| Loading Mechanism | fully automatic |
| Cooling | air/water |
| Mount | Enclosed naval gun mount |
| Barrel(s) | 2 |
| Gun Crew | 0 |
| Fire Control | remote |
| Builder(s) | Breda |
| 76MM/62-Caliber Lightweight Gun System (MK 75): | |
| Weight | Light |
| Mount | Enclosed naval gun mount |
| Barrel(s) | 1 |
| Gun Crew | 0 |
| Gun | 76mm/62-caliber |
| Ammunition | |
| Magazine Capacity | |
| Firing Rate | Rapid |
| Loading Mechanism | fully automatic |
| Cooling | Water |
| Range | |
| Fire Control | Remote |
| Builder(s) | |
| Notes |
Technical and operational evaluation of this gun system
was conducted at sea on USS Talbot (FFG-4). The Mark 75 was
provisionally approved for service use in September 1975.
The Naval Systems Division (NSD) of FMC Corporation and General
Electric Co. (Ordnance Systems Division) were both licensed by the
gun's designer, OTO Melara of La Spezia, Italy, and competed for
the right to manufacture the MK 75 in the United States. In 1975,
FMC/NSD subsequently won the competition. Since 1981, however, all
MK 75 buys have been competed between FMC/NSD and OTO Melaro has
won all competitive procurements. Because of performance, light
weight and low manning requirements, the MK 75 is suited for
installation on small combatants. Current usage includes one gun mount each for FFG-7 and PHM-1 class Navy ships, and one gun mount each for the WHEC-378 class and the WMEC-270 class Coast Guard cutters. The first United States produced gun mount was delivered in August 1978. |
| 5inch/54-Caliber Lightweight Gun System (MK 42): | |
| 5inch/54-Caliber Lightweight Gun System (MK 45): | |
| Gun | 5inch/54-cal. |
| Ammunition | |
| Magazine Capacity | |
| Firing Rate | 16 - 20 rpm |
| Loading Mechanism | fully automatic |
| Cooling | air |
| Range | |
| Weight | |
| Mount | Enclosed naval gun mount. |
| Barrel(s) | 1 |
| Gun Crew | 0 |
| Fire Control | Mark 86 Gun Fire Control System |
| Builder(s) | |
| Notes | This light weight gun system offers significant improvements in reliability and maintainability over 5-inch/54-caliber Mark 42 gun systems. The Mark 45 is controlled by the Mark 86 Gun Fire Control System. Deliveries began in 1971 and will continue through the 1990s for CG-47 and the DDG-51 classes. |
| 8inch Gun System (MK 71): | |
| Gun | 8inch |
| Ammunition | 8" 200 pound projectile |
| Magazine Capacity | 75 rounds |
| Firing Rate | 12 rpm |
| Loading Mechanism | fully automatic |
| Cooling | air |
| Range | |
| Weight | |
| Mount | Enclosed naval gun mount |
| Barrel(s) | 1 |
| Gun Crew | 0 |
| Fire Control | |
| Builder(s) | |
| Notes |
|
| Snark missile system: | |
| Talos missile system: | |
| Tartar missile system: | |
| Terrier missile sytem: | |
| STANDARD Surface Launch (SM-1 MR, SM-2 MR) Missile: | |
| Dimensions | Length: 14' 7"; Diameter: 13.5" |
| Wing Span | 3' 6" |
| Weight | SM-1: 1,100 pounds; SM-2: 1,380 pounds |
| Propulsion | Dual thrust, solid fuel rocket |
| Warhead | Proximity fuse, high explosive |
| Builder(s) | General Dynamics, Pomona Division Raytheon Motorola Morton-Thiokol Aerojet General and others |
| STANDARD Surface Launch (SM-2 ER) Missile: | |
| Dimensions | Length: 26.2'; Diameter: 13.5" |
| Wing Span | 5' 2" |
| Weight | 2,980 pounds |
| Propulsion | Two-stage, solid-fuel rocket -- sustainer motor and booster motor |
| Warhead | Proximity fuse, high explosive |
| Builder(s) | General Dynamics, Pomona Division Raytheon Motorola Morton-Thiokol Atlantic Research and others |
| Notes |
The SM-2 (ER) is an extended range area defense weapon for Leahy,
Belnap, Bainbridge, Truxton, and Long Beach class Terrier cruisers
with NTU conversion. In FY 1987, the Navy purchased 350 ER Standard
missiles; FY 1988 350 missiles; and FY 1989 400 missiles. The Standard family of missiles is one of the most reliable in the Navy's inventory. A two-model weapon which can be used against missiles, aircraft and ships, it first came into the fleet more than a decade ago. It replaces Terrier and Tartar and now is part of the weapons suit of more than 100 U.S. Navy ships. The SM-2 (MR) is a medium range defense weapon for Ticonderoga class Aegis cruisers; California and Virginia class Tartar nuclear cruisers with New Threat Upgrade (NTU) conversion; Kidd class Tartar destroyers with NTU conversion; and Oliver Hazard Perry class frigates with the SM-2 conversion. In FY 1987, the Navy purchased purchased 844 MR Standard missiles; FY 1988, 960 missiles; and FY 1989, 910 missiles. |
| Vertical Launch ASROC (VLA): | |
| Dimensions | Length: 192"; Diameter: 14.1" (body) |
| Weight | 1408 pounds |
| Propulsion | Solid Propellant Rocket |
| Warhead | MK 46 MOD 5 Torpedo |
| Guidance | Terminal Acoustic Homing with MK 46 Torpedo |
| Builder(s) | Loral Defense Systems Div. |
| Notes | VLA is an intermediate range, all-weather, quick reaction, ship launched ballistic anti-submarine weapon. It will be installed on VLS equipped DD 963, DDG 51 and CG 47 class ships. VLA, a replacement for the older ASROC missile on these ships, uses the MK 46 MOD 5 torpedo as its payload and will have increased range over the deck-launched ASROC. VLA will be replaced with the SEA LANCE missile when it becomes available. |
| MARK 6 Torpedo : | |
| Dimensions | Length: ? Diameter: ? |
| Weight | ? |
| Propulsion | steam speed: 46 kts. |
| Guidance | ? |
| Warhead | 750 lbs of TNT |
| Builder(s) | ? |
| Notes |
Mark 6 torpedo: Magnetic exploder: found to be defective in design, ordered inactivated in 6/43 and rely on backup contact exploder. Backup Contact exploder: found to be defective in design, modified at Pearl Harbor in late summer of 1943 |
| MARK 14 Torpedo (MK 14): | |
| MARK 37 Torpedo (MK 37): | |
| MARK 46 Torpedo (MK 46 MOD 5): | |
| Dimensions | Length: 102.357" (tube launch configuration) Diameter: 12.75" |
| Weight | 517.65 lbs. (warshot configuration) |
| Propulsion | Two-speed, reciprocating external combustion engine Mono-propellant (Otto fuel II) fueled |
| Guidance | Homing mode: Active or passive/active acoustic homing sonar Launch/search mode: Snake (HATS) or circle search (NRO) |
| Warhead | 98 lbs of PBXN-103 high explosive (bulk charge) |
| Builder(s) | Honeywell Inc. |
| Notes |
The MK 46 torpedo is a lightweight ASW torpedo designed
to attack high performance submarines. The MK 46 torpedo is presently identified as the NATO standard and since first introduced into the U.S. Navy fleet in 1967, has been acquired for employment by navies of several other countries. The MK 46 torpedo (presently available in Mods 1, 2, and 5) is designed to be launched from surface combatant torpedo tubes, ASROC missile, and fixed and rotary wing aircraft. Beginning in Fiscal Year 89, a major block upgrade program was initiated to enhance the performance of the Torpedo Mk 46 Mod 5 in a shallow water environment. Weapons incorporating these improvements are identified as Mod 5A and Mod 5A(S). The MK 46 Mod 5 torpedo is the backbone of the Navy's lightweight ASW torpedo inventory and is expected to remain in service until the year 2015. |
| MARK 48 Torpedo (MK 48 and MK 48 Advanced Capability (ADCAP)): | |
| Dimensions | Length: 19'; Diameter: 21" |
| Weight | (MK 48): 3434 pounds; (ADCAP): 3695 pounds |
| Speed | 28+ kts. |
| Range | 5+ miles; Depth: 1200'+ |
| Propulsion | Piston engine; pump jet |
| Warhead | 650 lbs high explosive |
| Builder(s) | |
| Notes |
The MK 48 is carried by all Navy attack and ballistic
missile submarines. The improved version, MK 48 ADCAP, is carried
by SSN 688 and SSN 637 class attack submarines and will be carried
in the future by the SEAWOLF class attack and OHIO class ballistic
missile submarines. Both of these weapons are designed to combat
fast, deep divine nuclear Submarines and high performance surface
ships. The MK 48 replaced both the MK 37 and MK 14 torpedoes in
anti-submarine and anti-ship roles, with the ADCAP supplementing
the MK 48 for use against the most advanced threat submarines and
surface ships. The MK 48 has been operational in the U.S. Navy since 1972, the MK 48 ADCAP became operational in 1988 and was approved for full production in 1989. The ADCAP has significantly increased capabilities over the MK 48. These capabilities allow its employment against the most advanced Soviet submarines. |
| MARK 50 Torpedo (MK 50): | |
| Dimensions | Length: 112"; Diameter: 12.75" |
| Weight | 750 pounds |
| Speed | 40+ kts. |
| Range | |
| Propulsion | Stored Chemical Energy Propulsion System |
| Guidance | Active/Passive acoustic homing sonar |
| Builder(s) | Honeywell Westinghouse |
| Notes | The MK 50 is an advanced lightweight torpedo for use against the faster, deeper-diving, and more sophisticated submarines being developed and operated by the Soviet Union. The MK 50 can be launched from all ASW aircraft, and from torpedo tubes aboard surface combatant ships. The MK 50 will eventually replace the MK 46 as the fleet's light weight torpedo with fleet introduction in the early 1990's. |