David
Sat January 3, 2004 8:47pm
|
M224 60mm Lightweight Mor
Function: To provide the company commander with an indirect-fire weapon.
Description: The M224 60mm Lightweight Mortar is a smooth bore, muzzle loading, high-angle-of-fire weapon. The cannon assembly is composed of the barrel, combination base cap, and firing mechanism. The mount consists of a bipod and a base plate which is provided with screw type elevating and traversing mechanisms to elevate/traverse the mortar. The M64 sight unit is attached to the bipod mount via a standard dovetail. An additional short range sight is attached to the base of the cannon tube for firing the mortar on the move and during assaults. It has a spring-type shock absorber to absorb the shock of recoil in firing.
History: The M224 replaced the older (WWII era) M2 and M19, 60mm Mortars. These weapons only possessed 2,200 yards of effective range. The M224 was designed to fire all types of the older ammunition, but its primary rounds are of the newer, longer-range type.
General Characteristics, M224 60mm Lightweight Mortar
Length:
40 inches (101.6 centimeters)
Weight:
46.5 pounds (21.11 kilograms)
Bore Diameter:
60mm
Maximum Effective Range:
2.17 miles (3490 meters)
Rates of Fire:
Maximum: 30 rounds/minute Sustained: 20 rounds/minute
Unit Replacement Cost:
$10,658
|
|
David
Sat January 3, 2004 8:47pm
|
M-252 Mortar
Function: Provides field artillery fire support for all Marine Corps Air Ground Task Force organizations.
Description: The M252 81mm Medium Extended Range Mortar is a crew-served, medium weight mortar which is highly accurate and provides for a greater range (4,500 meters to 5,650 meters) and lethality than the previous versions. The cannon has a crew-removable breech plug and firing pin. The muzzle end has a short tapered lead-in which acts as a blast attenuator device. The breech end is finned for better cooling. This mortar also uses the standard M64 mortar sight of the 60mm mortar, M224.
Background: This mortar replaced the previous Marine Corps 81mm mortar in 1986. The M252 is an adaptation of the standard British 81mm mortar developed in the 1970s. It is mostly commonly found in the mortar platoon of an infantry battalion. A Blast Attenuation Device (BAD) is attached to the muzzle of the weapon to reduce the blast effects on the mortar crew. The M252 is ideally suited to support airborne, air assault and light infantry units.
General Characteristics, M-252 Mortar
Length:
56 inches (142.24 centimeters)
Weight:
Mortar Assembly: 35 pounds (15.89 kilograms)
Bipod: 26 pounds (11.80 kilograms)
Baseplate: 25.5 pounds (11.58 kilograms)
Sight Unit: 2.5 pounds (1.14 kilograms)
Total: 89 pounds (40.41 kilograms)
Bore Diameter:
81mm
Maximum Effective Range:
5700 meters
Rates of Fire:
Maximum: 33 rounds per minute Sustained: 16 rounds per minute Elevation: 45 to 85 degrees
Minimum Range:
80 meters
Unit Replacement Cost:
$24,717
|
|
David
Sat January 3, 2004 9:38pm
|
MiG-21 Fishbed
Function: High performance Cold War era air combat and air superiority fighter.
History: Originally designed as a replacement for the MiG-19 Farmer, the Mikoyan-Gurevich Design Bureau passed on sophisticated technology in favor of pure airframe performance using solid, reliable technology which was easy to maintain. The end result was Soviet workhorse capable of performing a wide variety of missions, from close air support, to tactical aerial reconnaissance to air superiority and air combat. The MiG-21 design has been so successful that more MiG-21s have been produced than any other fighter aircraft and, 25 years after its introduction, it is still in production in a number of countries. The first prototype flew in 1955 and its existence was made public in 1956. Conceived as high performance daylight fighter-interceptor, the Fishbed sacrificed endurance and all weather capability for pure speed and aerobatic performance. Although the MiG-21 lacked the ordinance capacity of its contemporaries, the F-4 Phantom II and the F-105 Thunderchief, it was more maneuverable, and because of its simple design, it was both easier and cheaper to maintain by the cash poor countries which purchased it.
Since its introduction over 15 different variants of the Fishbed have been produced. Initial prototypes MiG-21s (Fishbed-B) were armed with two NR-30 30mm cannons but this was reduced to one in later (Fishbed-C) production runs as the Soviet Union followed the West in converting fighters from gun to missile platforms. In addition to eliminating one of the cannons, the Fishbed-C had an increased internal fuel capacity and launch rails for two AA-2 Atoll IR Missiles or rocket pods for ground support missions. The Fishbed-D eliminated the internal cannon armament while increasing internal fuel load as well as redesigning the Spin Scan radar located in the movable nose cone. The Fishbed-E is essentially a sub variant of the D model, incorporating a number of minor modifications, including the reintroduction of a cannon armament in the form of a GP 9 gun pod. The Fishbed-F was the final "first generation" production aircraft. In addition to improvements in the fuselage, internal fuel capacity and control surfaces, the F model incorporated a new radar which allowed it to fire semi-active medium range radar homing air to air missiles.
The "Second Generation" MiG-21s represented a divergence from the original lightweight fighter concept. These aircraft would be characterized by larger fuel loads, more advanced electronics, greater ordnance capacity, and better performance. The first of the "Second Generation" aircraft were the Fishbed-H, a dedicated reconnaissance and offensive electronic warfare variant, and the Fishbed-J, which dispensed with the GP 9 pod in favor of a single, internally mounted GSh-23L 23mm cannon. Wing pylons were also increased from two to four. The last of the "Second Generation" MiG-21s introduced was the Fishbed-H which was similar to the J but featured a greatly enlarged dorsal spine which housed additional fuel. Unfortunately this increased weight so reduced performance that its carrying capacity had to be cut by 50 percent.
"Third Generation" Fishbeds represent the final iteration of MiG-21 evolution. Though "Third Generation" aircraft represent a real improvement over earlier versions, in comparison to current aircraft, the lack of a Beyond Visual Range (BVR) missile capability, poor endurance and poor slow speed/high G handling limit its combat utility. The Fishbed-L was the first of the next generation aircraft, incorporating numerous technological improvements, and was designed with low altitude performance in mind. Though the MiG-21 remains in limited production in a number of countries, the Fishbed is likely to remain in service for many more years, thanks to an aggressive aftermarket product improvement program. Many countries, such as Israel, Russia, India, and China offer aftermarket upgrade packages, where countries can refit older versions of the MiG-21 with more advanced, to include Western technology, components.
General Characteristics, MiG-21 Fishbed
Designer:
Mikoyan-Gurevich Design Bureau
Power Plant:
Fishbed-F: one Tumanskii R-11F2S-300 turbojet rated at 8,600 pounds thrust dry and 13,613 pounds thrust on afterburner
Fishbed-J: one Tumanskii/Gavrilov R-13-300 turbojet rated at 8,972 pounds thrust dry and 14,307 pounds thrust on afterburner
Fishbed-L: one Tumanskii R-25-300 turbojet rated at 9,038 pounds thrust dry and 15,653 pounds thrust on afterburner; the R-25-300 is capable of producing 21,825 pounds of thrust above Mach 1 and up to 13,000 feet for periods of up to three minutes
Length:
12.285 meters (40 feet, 3.9 inches)
Height:
4.125 meters (13 feet, 6.2 inches)
Wingspan:
7.154 meters (23 feet, 5.7 inches)
Speed:
Fishbed-F: 2,125 kmh (1,320 mph) at 11,000 meters (36,090 feet)
Fishbed-J: 2,230 kmh (1,385 mph) at 11,000 meters (36,090 feet); maximum level speed at sea level 1,300 kmh (807 mph)
Fishbed-L: 2175 kmh (1,351.5 mph) at 13000 meters (42,650 feet)
Ceiling:
Fishbed-F: 19,000 meters (62,335 feet)
Fishbed-J: 18,200 meters (59,711 feet)
Fishbed-N: 17,500 meters (57,415 feet)
Weight:
Fishbed-F: 5,350 kilograms (11,795 pounds) empty
Fishbed-J: 5350 kilograms (11,795 pounds) empty
Fishbed-N: 5450 kg (12,015 pounds) empty
Maximum Takeoff Weight:
Fishbed-F: 9,080 kilograms (20,018 pounds)
Fishbed-J: 9,400 kilograms (20,723 pounds)
Fishbed-N: 10,400 kilograms (22,928 pounds)
Range:
Fishbed-F: Maximum ferry range with one external fuel tank 1300 kilometers (808 miles)
Fishbed-J: Maximum ferry range with three external fuel tanks 1,800 km (1,118 miles)
Fishbed-N: Maximum ferry range with one external fuel tank 1,470 km (913 miles)
Crew:
One
Armament:
Fishbed-F: One NR-30 30mm cannon in an external pod plus either two AA-2 short range Infrared homing air to air missiles or up to 500kg (1,100 pounds) of external ordnance on two pylons
Fishbed-J,N: One GSh-23L internally mounted 23mm cannon plus either four air to air missiles or up to 2000 kilograms (4,409 pounds) of external ordnance carried on four pylons
Date Deployed:
1956 (Fishbed-C)
|
|
David
Sat January 3, 2004 9:38pm
Rating: 10
|
Su-25 Frogfoot
Function: Dedicated Close Air Support (CAS) ground attack fighter.
History: Introduced in 1980, the Su-25 Frogfoot was the first dedicated ground attack aircraft produced by the Soviet Union since the World War Two era propeller driven Il-2 Shturmovik. drawing heavily on lessons learned by the American Air Force during the vietnam war, and mirroring the performance of the American A-10 Warthog, the Frogfoot is a rugged aircraft capable of accuratly delivering a heavy payload from low altitude and surviving in the low level, high threat forward area environment. Though the Sukhoi Design Bureau originally sought to rely on speed to survive, it was determined that increased speed reduced the low level battlefield effectiveness of the aircraft. In short, if the aircraft was to perform its job effectivly, it would have to be capable of operating at low speeds; speed would be sacrificed for low speed maneuverability and heavy armor.
After several design changes, the first prototypes were approved in 1980. The first production Frogfoots were equipped with twin multi-fuel non afterburning turbojet engines, a twin barreled internally mounted 30mm cannon, titanium armor around the pilot and control surfaces, and foam filled, non-explosive self sealing fuel cells. The Su-25 was equipped with eleven underwing and under body hard points, was capable of delivering 4000 kilograms (8,818 pounds) of ordnance and could be operated off of unimproved dirt strips.
Following combat experience in Afganistan, an improved version, the Frogfoot-B, was fielded in 1984. The B model was a production modified version of the two seat Frogfoot-A trainer. The second seat was removed, as was the internal gun, and additional fuel, armor, and avionics were installed, in addition to an improved 30mm cannon, mounted in an external pod. In addition, the Frogfoot's lack of all weather, night time capability was addressed by incorperating a Forward Looking Infra Red (FLIR) low light navigation system as well as a TV camera and laser designator, spot tracker and rangefinding package.
Although the Frogfoot has been out of production for a number of years, it still remains in front line service with Russia's Frontal Aviation as well as many export nations, including Iraq.
General Characteristics, Su-25 Frogfoot
Designer:
Sukhoi Design Bureau
Power Plant:
Two MNPK Tumanskii R-195 turbojets
Thrust:
9,921 pounds thrust each
Length:
15.53 meters (50 feet, 11.5 inches)
Height:
4.80 meters (15 feet, 9 inches)
Wingspan:
14.36 m (47 feet, 1.4 inches)
Speed:
950 kmh (590 mph) at sea level
Date Deployed:
1980
Ceiling:
7,000 meters (22,965 feet)
Weight:
9,800 kilograms (21,605 pounds) empty
Maximum Takeoff Weight:
18,600 kilograms (41,005 pounds)
Range:
Combat radius 495 kilometers (308 miles)
Crew:
One
Armament:
One AO-17A 30-mm twin barreled cannon
4,000 kilograms (8,818 pounds) of external ordinance including missiles, rockets, gravity bombs, and guided munitions carried on 11 hardpoints
|
|
David
Sat January 3, 2004 9:38pm
|
Shenyang J-8 (F-8 Finback
Function: Twin-engined, single-seat aircraft is primarily used for air combat, with the capability of ground attack.
History: Introduced in 1964, the J-8 was the first People's Liberation Army Air Force (PLAAF) aircraft utilizing a wholly Chinese design. While similar in configuration to the Soviet MiG-21 or the Chinese J-7, the J-8 airframe has been enlarged to accommodate two engines. Although the design was approved in 1964, prototype production was not completed until 1969. Because of the civil unrest caused by the Cultural Revolution (1966-76), the prototypes would see only limited flight activity through 1976, delaying production further. Production of the J-8 began in December 1979, with very few airframes actually entering service. These first-run aircraft were equipped with a single axial air intake supplying air to both engines, with a centrally mounted ranging radar, which gave the aircraft an appearance similar to the Mig-21/J-7. These aircraft were also equipped with two Type 30 30mm cannons and four under wing hardpoints, capable of firing the PL-2B short-range air-to-air missile. First-run production was completed in 1987.
The second run J-8 I "Finback A" entered production in 1985. Similar to the original J-8, the J-8 I had an improved radar which gave it all-weather capability. In addition, the two 30mm cannons were replaced by a single twin-barreled 23mm cannon. Production was halted in 1987 after some 100 aircraft were built (including original J-8 aircraft converted to the J-8 I design).
The completely redesigned J-8 II "Finback B" was first flown in 1984 and made public in 1986. The forward section of the airframe has been completely redesigned, replacing the single combination air intake-radome with two separate intakes, mounted laterally on the fuselage just aft of the cockpit, and a solid nose housing the aircraft's search radar. The solid nose also increases the amount of space available for additional after-market avionics. The J-8 II also incorporates a ventral stabilizer fin for increased maneuverability, which can folded for takeoff and landing. The export model of the J-8 II, designated the F-8 II, has improved avionics, to include digital electronics, a Heads Up Display (HUD), and Doppler radar, and engines, along with leading edge slats and in-flight refueling capabilities, giving it improved performance characteristics.
The J-8 IIM is a private venture (sponsored by Shenyang Aircraft Company) to improve the performance, and marketability, of the Basic J-8 II design. The J-8 IIM is capable of launching a variety of air-to-air and air-to-ground ordnance, including the PL-8, R-27/AA-10 and PL-5B. In addition, conventional iron bombs can be carried on seven hardpoints. The J-8 IIM also incorporates the advanced Russian made Zhuk-8II (FG-8) look-down, shoot-down radar, which replaces the older Chinese Type-208 radar. The Zhuk-8II has a range of 70 nautical miles, is able to track up to 10 targets at once and engage 2 targets simultaneously with radar-guided missiles such as the AA-10, as well as to launch anti-ship missiles such as the Kh-31. While the J-8 IIM also incorporates improved engines, the J-8 IIM is actually heaver than the baseline model, so aircraft range and performance are down slightly. Though the J-8 IIM completed its first test flight in 1998, none have been exported.
The most recent variant of the J-8 introduced, the J-8D, appears to be a basic J-8 II modified with a fixed in-flight refueling probe. In addition, it would seem that the avionics package has been upgraded to allow the ability to fire the PL-8 IR missile and the PL-11 semi-active radar guided missile.
Description: The basic J-8 design is very similar in appearance to the Soviet MiG-21 and Chinese J-7 aircraft, with the modified delta wing, swept horizontal and vertical stabilizers and central combination air intake-radar housing. The J-8's laterally mounted twin engines, however, readily give it away, the twin exhausts easily visible below and aft of the vertical stabilizer. The J-8 II replaces the MiG-21 forward section with a completely new design, incorporating the same single seat stepped cockpit, but with a solid nose and two laterally mounted, one on each side of the fuselage, square air intakes. The back half of the J-8 II, however, remains largely unchanged from the original J-8 design.
General Characteristics, Shenyang J-8 (F-8 Finback)
Country:
People's Republic of China
Designation:
Jian-8 Finback
Type:
Intercept
Builder:
Shenyang Aircraft
Power Plant:
Two open 13A-II turbojets at 14,815 pounds thrust
Length:
70 feet, 10 inches (21.6 meters)
Wingspan:
30 feet ( 9.3 meters)
Weight:
Empty: 21,600 pounds (9,820 kilograms)
Normal Takeoff: 31,500 pounds (14,300 kilograms)
Maximum Takeoff: 39,200 pounds (17,800 kilograms)
Speed:
Maximum Speed: 1,450 mph (2,340 kmh, Mach 2.2)
Cruising Speed: 800 mph (1,300 kmh)
Ceiling:
18-20,000 meters
Range:
Combat Radius: 2,500 miles (800 kmh)
Cruise Radius: 800 miles (1,300 kilometers)
Ferry Range: 1,400 miles (2,200 kilometers)
Internal Fuel Capacity:
3994 kilograms
Armament:
Two 23mm cannons (J-8 only; not found on J-8II)
One underfuselage hardpoint
Six underwing hardpoints for fuel, bombs, rockets or missiles
Four PL-2 or PL-7 and 800 L drop tank (680 nm)
Two PL-2 or PL-7 and two 480 L drop tanks and one 800 L drop tank (741nm)
Sensors:
Izmurd raging radar
RWR
Ballistic bomb sight
Crew:
One
|
|
David
Sat January 3, 2004 10:15pm
|
BMP-1 APC
Function: Soviet Union's first tracked Armored Personnel Carrier.
Description: The BMP-1 is a tracked, amphibious, fully enclosed armored personnel carrier armed with a 73mm smoothbore cannon, one 7.62mm coaxial machine gun and the AT-3 SAGGER antitank guided missile (ATGM). The BMP-1 represents a significant improvement over the wheeled BTR series in all aspects, including mobility, firepower, and survivability. Fielded in 1966, the BMP-1 has been modified to serve as a common chassis for a number of additional vehicle types. No longer in production, the BMP-1 has been surpassed by the BMP-2 and 3 in both service in the Russian army as well as export abroad.
General Characteristics, BMP-1 Armored Personnel Carrier
Transmission:
Manual with five forward gears and one reverse
Engine:
6 cylinder diesel engine producing 290 horsepower
Length:
22 feet (6.7 meters)
Width:
9 feet (2.74 meters)
Height:
7 feet (2.13 meters)
Combat Weight:
14 tons
Cruising Range:
372 miles (600 kilometers)
Speed:
Maximum: 40 mph (65 kph), or 45 mph (70 kph) for limited periods
Cross Country: 28 mph (45 kph)
Obstacle Crossing:
Trench: 8.2 feet (2.5 meters)
Slope: 31 degrees
Crew:
Three: driver, gunner and commander (who serves as squad leader when the the infantry squad dismounts)
Armament:
Main: 73mm 2A20 smoothbore cannon
Secondary: One AT-3 SAGGER ATGM, one 7.62mm PKT coaxial machine gun
Ammunition:
40 73mm cannon rounds (fin stabilized HEAT only)
2,000 7.62mm machine gun rounds
Introduction Date:
1966
Variants:
BMP-A: Also known as the Model 1966, this was the original version of the BMP. It has a shorter bow compared to its successor, the BMP-1 and does not have a Nuclear, Biological, Chemical (NBC) protection system.
BMP-1: Also known as the Model 1976 this was the base production model from which all variants were designed.
BMP-1K: The command variant of the BMP-1. It differed from the BMP-1 in that it carried additional communications equipment and had the rifle firing ports welded shut. In addition the troop compartment was redesigned to accommodate folding tables and map charts. Can be used as a battalion level command vehicle.
BMP-1P: The AT-3 SAGGER ATGM has been replaced by the AT-4 SPIGOT ATGM. Additionally, smoke grenade launchers have been mounted on the turret rear.
BMP-1PK: Command variant of the BMP-1P. Similar to the BMP-1K, it has additional communications equipment and has been modified to serve as a command vehicle. BMP-R: Also known as the BRM, BRM-1 and BMP M1976, this variant serves as a cavalry recon vehicle. The turret is larger and has had ATGM launcher removed. The back deck of the hull has been redesigned with two smaller hatches rather than the four large ones found on the BMP-1.
BRM-1K: Also known as the BMP M1976/2 this variant is based off of the BRM-1 with the PSNR-5K (NATO designation TALL MIKE) battlefield surveillance radar mounted in the rear section of the turret. Also included in the vehicle's sensor package are the DKRM-1 laser rangefinder, ARRS-1 location device, IMP mine detector and 1PN33B night vision devices. For navigation the BRM-1K uses the TNA-1, IG11N gyro-compass and the 1T25 survey device.
BMP KShM: Also known as the BMP M1978 it is a heavily modified BMP-1K with additional communications gear and a telescoping radio antenna for increased transmission range.
BMP-SON: Also known as the PRP-3, this is a BMP-1 modified to serve as an artillery reconnaissance and fire support vehicle. The turret has been redesigned to include two forward opening crew hatches equipped with observation periscopes as well as a large spotting optics. A large telescoping optical device is mounted on the left rear corner of the turret. The 73mm gun has been removed and replaced by a 7.62mm machine gun. Mounted on the rear of the vehicle is the SMALL FRED (NATO designation) battlefield surveillance radar. As with the command variants, the BMP-SON has an augmented communications package. The BMP-SON has a crew of 5.
PRP-4: This is essentially an upgraded and improved version of the PRP-3 (BMP-SON). Externally, the only difference is an additional fairing on the right side of the turret.
IRM: Amphibious Engineer Reconnaissance Vehicle. Based on the BMP-1, it uses the BMP-1 engine and suspension in a new hull design. Designed to perform specialized engineer missions such as mine detection and river bottom reconnaissance the IRM has two retractable mine detection devices mounted low on the bow and rapidly deployable snorkel. The IRM is propelled through the water via two shrouded propellers.
BMP-PPO: A heavily modified BMP-1 designed to serve as a mobile training center. The turret has been removed and eight roof mounted cupolas each equipped with a TNPO-170 and type MK-4 observation device, have been installed for trainees under instruction.
OT-90: Czechoslovakian version of the BMP-1. The turret has been replaced with the standard Czechoslovakian APC turret, equipped with a 14.5mm machine gun and a 7.62mm machine gun, found on the OT-64 8x8 wheeled APC.
BVP-1: Czechoslovakian produced BMP-1.
DP-90: Maintenance/recovery version of the OT-90.
MP-31: Air defense version of the BMP-KShM mobile command post.
MU-90: Mine laying version of the OT-90. The turret has been removed and the opening covered by sheet steel.
SVO: Mine clearing version of the BMP-1. The turret has been removed and a hedgehog type launcher has been installed in the troop compartment.
VPV: Maintenance/recovery version of the BMP-1. The turret and troop hatches have been removed and a crane has been installed on the roof of the troop compartment.
VP-90: Reconnaissance version of the OT-90. Similar to the BMP-R in all other respects.
|
|
David
Sat January 3, 2004 10:15pm
|
T-62 MBT
Function: Soviet front line MBT during the 1960s.
Background: The T-62 was introduced in 1961 to replace the T-55 as a Soviet front line main battle tank. In many respects, the T-62 represents a product improvement upgrade of the T-55; the T-62 uses the same 580hp V-12 diesel engine, the track, suspension, and drive train arrangement are essentially the same. The initial-run T-62 also shared the same NBC protection system and active infrared gunner's sight as the T-55. The T-62 uses the same fording components as the T-55 and is capable of fording to a depth of 1.4m without modification and to 5.5m with the snorkel kit. The T-62 is capable of producing onboard smoke by injecting vaporized diesel fuel directly onto the engine exhaust.
The T-62's real improvement lay in its 115mm smoothbore, high velocity cannon. With a muzzle velocity of over 1,600m/s, the T-62 has a nearly flat trajectory through its entire effective range, making the gun very accurate. Later production models incorporate a true NBC filtration/over-pressurization system, thus eliminating the need for the crew to wear protective masks while inside the tank, as well as a passive IR gunner's sight which eliminated the need for active infrared search lights which would reveal the location of the illuminating tank.
Although the Soviet Union ceased production of the T-62 in 1975, the T-62 still remains in front-line service with a number of countries world-wide.
Description: The T-62 is similar in appearance to the T-55. The T-62 uses the same "live track" design as the T-55. There are 5 large cast road wheels, with a distinctive gap between the third and fourth and the fourth and fifth road wheels. The track is all steel, the idler wheel is to the front, the drive sprocket is to the rear and there are no return rollers.
The turret is more egg or pear-shaped than dome-shaped, as with the T-55, and the attached infantry hand rails, if present, are both curved, as opposed to the straight and curved rails on the T-55.
The main IR searchlight is mounted on top of the turret, to the right of the main gun, as with the T-55, with one secondary searchlight mounted below the main light to the right of the gun and one mounted on the commander's cupola on the left side of the turret.
The 115mm smoothbore cannon uses the same trunion arrangement as with the T-55, substituting an armored mantlet for a canvas weather-resistant cover. The cannon has a bore evacuator mounted one third of the way down the gun tube and may be equipped with a thermal sleeve.
The T-62 employs the same coaxial PKT-T 7.62mm machine gun as the T-55 and is mounted to the right of the main gun. The 12.7mm DShK anti-aircraft machine gun is mounted at the loader's station.
As with the T-55, the T-62 does not use armored fuel cells. Instead, the fuel is stored in exposed tanks on the track fenders. The engine exhaust is expelled out the left rear side of the hull. Auxiliary fuel tanks may be attached to the rear of the hull.
General Characteristics, T-62 Main Battle Tank
Manufacturer:
Soviet Union
Transmission:
Automatic
Engine:
620hp liquid cooled V-12 diesel
Length. Gun Forward:
21.55 feet (6.63 meters)
Width:
11.44 feet (3.52 meters)
Height:
7.8 feet (2.4 meters)
Combat Weight:
41.5 tons
Cruising Range:
450 kilometers (650 kilometers with additional fuel tanks)
Speed:
Maximum: 28 mph (45 kph)
Fording:
Without Preparation:
4.55 feet (1.4 meters)
With Snorkel:
17.88 feet (5.5 meters)
Crew:
Four (Loader, driver, gunner, Tank Commander)
Armament:
Main:
115-mm smoothbore gun, 2A20
AT-10 Sheksna Cannon launched ATGM
Secondary:
One 12.7mm DShK anti-aircraft machine gun (loader's station)
One 7.62mm PKT-T coaxial machine gun
Ammunition:
40 main gun rounds, typically 12 HVAPFSDS rounds, 6 HEAT rounds, and 22 HE rounds
Sensors:
Drozd APS (T-62D)
Introduction Date:
1961
Variants:
T-62A: First production model of the T-62. Incorporates the 12.7-mm DShK anti-aircraft machine gun, which is mounted at the loader's station, and an improved two-axis gun stabilization system that gives the gunner limited a shoot-on-the-move capability.
T-62K: Command variant. In addition to having increased radio capabilities, the "K" model also possesses an inertial land navigation system. Using a gyroscopic compass and distance calculator this navigation system allows the commander to plot his location from a known point as well as display direction and distance to a plotted point.
T-62M: The T-62M is essentially an "A" model upgraded to the T-55M standard. Added the Soviet made Volna fire control system (dual-axis stabilization, laser range finder) as well as a cannon launched ATGM (AT-10 Sheksna.) Upgrades in armor protection include the 180o "bra" armor belt on the front half of the turret, track side skirts, and smoke grenade launchers.
T-62M1: "M" model without the through cannon ATGM capability. "-1" variants have replaced their standard power plant with the 780hp V-46 12 cylinder diesel engine from T-72 MBT.
T-62D: Variant with the Drozd APS in place of Explosive Reactive Armor (ERA.) Developed by the Soviet Union in 1977, the Drozd system was designed as an active defense against ATGMs and anti-tank grenades. The system was based on a number of millimeter-wave radar transceivers situated around the turret. The radar sensors would detect the approach of an ATGM and fire off short-ranged fragmentation rockets that were intended to shred the incoming missile. To prevent accidental discharge, the system was equipped with a filter to react only to objects flying at characteristic ATGM speeds. The four-barreled launchers were located on the forward part of the turret and only provided protection for the front 60? portion of the turret. To change the covered arc of coverage the crew would have to rotate the turret and orient the coverage cone on the threat.
T-62MK: Command variant of the T-62M.
T-62MV: "M" variant with ERA (either Kontakt or Kontakt-5 second generation) in place of the bra armor.
|
|
David
Sat January 3, 2004 10:15pm
|
T-80 MBT
Function: Current Russian front line main battle tank (MBT).
Description: The T-80 MBT is a continuation of the T-64/T-72 series, retaining many similar features of the previous tanks. It is similar to the T-72 in that it retains the low silhouette, centrally mounted round turret with the commander seated to the right of the main gun and the gunner on the left. As with the T-72 the T-80 retains the use of the automatic loader, feeding ammunition from a 27 round circular magazine around the turret ring. Attached to the hull below the front slope is a toothed dozer blade. Beneath the blade are attachment points for the KMT-6 mine plow. The T-80 is the first Soviet design to incorporate a laser rangefinder as well as a gas turbine engine for increased automotive performance. The T-80 is currently in service with the Russian army and is slowly being replaced by the T-90.
General Characteristics, T-80 Main Battle Tank
Manufacturer:
KBTM, Omsk, Russian Federation
XKBM, Kharkov, Ukraine (T-80UD and T-84)
Transmission:
Automatic
Engine:
GTD-1250 gas turbine, 1250 horsepower (T-80U, T-80 originally equipped with the GTD-1000 delivering 1,100 horsepower)
Length. Gun Forward:
31.69 feet (9.66 meters)
Width:
12.00 feet (3.60 meters)
Height:
7.21 feet (2.20 meters)
Combat Weight:
46 tons
Cruising Range:
350 kilometers (600 kilometers with additional fuel tanks)
Speed:
Maximum: 43 mph (70 kph)
Cross Country: 30 mph (48 kph)
Obstacle Crossing:
Trench: 9.35 feet (2.85 meters)
Slope: 32 degrees
Fording:
Without preparation: 5.9 feet (1.8 meters)
With Snorkel: 16.4 feet (5 meters), or (39.4 feet (12 meters) with BROD-M system
Crew:
A three-man crew composed of a driver, gunner, and tank commander
Armament:
Main: 125mm 2A46M-1 main gun
Secondary: One 12.7mm NSVT anti-aircraft machine gun (commander's station), one 7.62mm PKT coaxial machine gun
Ammunition:
45 125mm Cannon rounds (combination of kinetic energy (SABOT), High Explosive Anti Tank (HEAT) shaped charge, High Explosive-Fragmentation (HE-FRAG), cannon launched AT-8 ATGM)
450 12.7mm machine gun rounds
1,000 7.62mm machine gun rounds
Sensors:
Shtora-1 countermeasures suite (T-80UK, T-80UM1)
Arena active protection system (T-80UM1, T-84)
Introduction Date:
1978
Variants:
T-80: Original production version. Fielded in 1978, equipped with the GTD-1000 gas turbine engine delivering 1100 horsepower. Utilized the same 125mm smoothbore cannon (2A46M-1) as the T-72 series but capable of firing the cannon launched, 9M177 Kobra ATGM (NATO designation AT-8 SONGSTER.) Tank is equipped with a 7.62mm PKT machine gun coaxial mounted on the right side of the cannon and a 12.7mm NSV machine gun mounted in the commanders cupola.
T-80B: First upgrade. Incorporates composite K ceramic armor in turret design to improve defense against kinetic energy (KE) penetrators. T-80BK is the command variant of the B model and has increased communications equipment. T-80BV: B model equipped with first generation reactive armor. At the time of its introduction, the application of reactive armor made the T-80 immune to all NATO ATGMs in production. The T-80BVK was the command variant of the T-80BV.
T-80U: First observed in 1989. Designated the M1989 SMT (Soviet Medium Tank). Modifications include a new turret design with improved frontal armor as well as the application of second generation explosive reactive armor. The AT-8 has been replaced by the cannon launched, laser guided 9M119 Refleks ATGM (NATO designation AT-11 SNIPER). Engine has been upgraded to the more powerful GTD-1250 gas turbine producing 1250 horsepower. The commander's weapon station has been redesigned to allow the firing of the 12.7 NSVT machinegun from within the turret. The T-80UK is the command variant of the T-80U. In addition to additional communications equipment, the T-80UK also fields the Shtora-1 countermeasures suite, an automated system combining an infrared jammer, laser warning system, and grenade discharging system.
T-80UM1: Incorporates new gunner's thermal sight as well as the Shorta-1 countermeasures suite and new Arena active ATGM protection system. Use of the Arena system precludes the need for the Kontakt-5 second generation reactive armor and so it has been removed.
T-80UD: Esentially a Ukrainian built version of the Russian T-80U. Major differences include the replacement of the gas turbine engine with a GTF V-12 diesel engine producing 1000 horsepower and the use of first generation reactive armor in pmace of the second generation Kontakt-5 ERA.
T-84: An improved version of the Ukrainian T-80UD incorporating the 6TD-2 diesel engine generating 1200 horsepower. In addition, the T-84 fields the Shtora-1 countermeasures suite and the ARENA active antimissile defensive system as well as the Ukrainian produced KBA-3 125mm smoothbore cannon and 28 round autoloader.
|
|
David
Sat January 3, 2004 10:15pm
|
T-55 MBT
Function: Soviet front line MBT during the 1950s.
Background: Introduced in 1949, the T-54/55 is in service with more countries world-wide and in greater numbers than any other tank manufactured since World War II. The first new tank of the post-World War II Soviet Union, the T-54/55 can trace its lineage back to the IS series Stalin heavy tanks and the revolutionary T-34 medium tanks.
The T-54 entered production in the Soviet Union in 1947, and was fielded with Soviet ground forces in 1949. By 1958, the T-54 had undergone a number of improvements and modifications and was re-designated the T-55. The T-55 represents an evolution of the T-54 rather than a completely new design.
The T-55 was produced by the Soviet Union through 1981. In addition, the T-55 was also produced in China (where it was designated the Type 59), Czechoslovakia, and Poland. The T-55 is capable of fording to a depth of 1.4m without modification and to 5.5m with the addition of a snorkel kit. The T-55 is capable of producing onboard smoke by injecting vaporized diesel fuel directly onto the engine exhaust.
Though time and technology have rendered the T-55 obsolete as a front-line main battle tank, large numbers of 54/55s remain in service with militaries world-wide. The T-55 saw service in Hungary in 1956, Czechoslovakia in 1968, and in Syria in 1970. In addition, it was the main battle tank used by the Arab forces during the 1967 and 1973 Arab-Israeli wars. During the 1970s the T-54/55 also saw extensive use during the border wars in Africa. Since so many T-54/55s remain in service, many countries, such as Israel, Pakistan, and India offer upgrade packages to rebuild existing tanks using more modern, and in many cases Western, fire control components, thus extending their usable life even further.
There are currently seven production models of the T-54/55, and more than a dozen variants.
Description: The T-54/55 tank follows a conventional layout, with a dome-shaped turret centrally located on the hull and the engine mounted in the rear. The 54/55 has a crew of four; driver (located in the left hand side of the hull, forward of the turret) loader (right hand side of the turret) tank commander and gunner (both located on the left side of the turret.
The T-54/55 can be identified by the distinct gap between the first and second of its five large cast road wheels. The 54/55 uses steel track (this may be substituted for padded track in modified versions), a torsion bar "live track" suspension with no return rollers and a rear mounted drive sprocket. The T-55 does not use armored fuel cells. Instead, the fuel is stored in exposed tanks on the track fenders. The engine exhaust is expelled out the left rear side of the hull.
The 100mm cannon is centrally mounted in the turret. The cannon trunions are not protected by an armored mantlet, but rather a canvas sleeve that protects the mechanism from the elements. There is no fume extractor on the T-54, while the T-55 has a bore evacuator mounted on the muzzle of the gun.
There are two hatches on the top of the turret (loader's and tank commanders.) Both hatches open forward. In the T-54 the 12.7mm DShK AA MG is mounted in the commander's station; on the T-55 ("A" version and beyond) the machine gun is located in the loader's position.
Two infantry support rails (one straight, one curved) are affixed to the turret sides. These may be removed to accommodate ERA, APS or applique armor packages. If present the main IR searchlight will be mounted on top of the turret (to the left of the gun.) An additional searchlight may be mounted on the commander's hatch. If present, the laser rangefinder will be mounted externally on the top of the main gun itself.
Because the T-55 does not use synchronized optics for the main gun, another identifying characteristic of the T-55 is the large sighting oval on the left hand side of the turret next to the gun mantlet. The aperture on the right hand side of the turret is the firing port for the coaxial PKT-T machine gun.
General Characteristics, T-55 Main Battle Tank
Manufacturers:
Soviet Union, Czechoslovakia, and Poland
Transmission:
Automatic
Engine:
580hp liquid cooled V-12 diesel
Length. Gun Forward:
20.15 feet (6.20 meters)
Width:
11.7 feet (3.60 meters)
Height:
7.54 feet (2.32 meters)
Combat Weight:
40.5 tons
Cruising Range:
500 kilometers (715 kilometers with additional fuel tanks)
Speed:
Maximum: 31 mph (50 kph)
Off road: 22 mph (35 kph)
Fording:
Without Preparation:
54.5 feet (1.4 meters)
With Snorkel:
17.9 feet (5.5 meters)
Crew:
Four (Loader, driver, gunner, tank commander)
Armament:
Main:
100mm rifled gun, D-10T2S
AT-10 Sheksna Cannon launched ATGM
Secondary:
One 12.7mm DShK anti-aircraft machine gun (loader's station.)
One 7.62mm PKT-T coaxial machine gun
Ammunition:
43 main gun rounds.
Sensors:
Drozd APS (T-55AMD, T-55AD Drozd)
Introduction Date:
1949
Variants:
T-54A: The initial production model of the T-54 tank. It has a bore evacuator at the end of the barrel for the 100mm gun, a stabilization system for the main gun (in the vertical plane only) and deep fording equipment. The turret is also equipped with a coaxially mounted PKT-T 7.62mm machine gun, and the tank commander's station is equipped with a 12.7mm DShK anti-aircraft machine gun.
T-54AK: Command tank variant of the T-54. The AK variant is a T-54A with long-range radio transmitting capability. The Polish model is the T-54AD.
T-54B: Equipped with active infra-red sights, giving the tank a limited night time fighting ability.
T-55: Essentially an upgraded T-54. The T-55 incorporates a more powerful water-cooled V-12 diesel engine. The cruising range has also been increased from 400km to 500km (range can be increased to 715km with the addition of auxiliary fuel tanks mounted on the rear of the hull.) The T-55 uses a new turret design, which incorporates an improve ventilation design and hatch design. The initial production T-55 did not have the 12.7mm DShK AA MG.
T-55A: Incorporates a new anti-radiation lining in the turret as well as a Nuclear Biological Chemical (NBC) air filtration system. The T-55A Model 1970 saw the re-introduction of the 12.7mm DShK AA MG, though it is now mounted at the loader's station.
T-55M: Added the Soviet made Volna fire control system (dual axis stabilization, laser range finder) as well as a cannon launched ATGM (AT-10 Sheksna.) Upgrades in armor protection included the addition of side skirts on the track, applique armor, as well as smoke grenade launchers. T-54s upgraded to the "M" standard were designated the T-54M
T-55AM: Adds an armor band around the front of turret for 180? coverage (similar to the T-72B "Dolly Parton" variant.)
T-55AMV: Substitutes Explosive Reactive Armor for the "bra" armor belt of the "AM" variant. Some variants have replaced the standard T-55 V-12 diesel with the 780hp V-46 12 cylinder diesel engine from T-72 MBT.
T-55AM2B: Czech version of T-55AMV with Czech built Kladivo fire control system.
T-55AM2: Variant of the T-55AM that incorporates all of the upgrades of the "M" and "AM" except for the Volna fire control system and cannon launched AT-10 ATGM.
T-55AM2P: Polish version of T-55AMV. Equipped with the Polish built Merida fire control system.
T-55AMD: T-55AMV incorporating the Drozd Active Protection System (APS) instead of ERA. Developed by the Soviet Union in 1977, the Drozd system was designed as an active defense against ATGMs and anti-tank grenades. The system was based on a number of millimeter-wave radar transceivers situated around the turret. The radar sensors would detect the approach of an ATGM and fire off short-ranged fragmentation rockets that were intended to shred the incoming missile. To prevent accidental discharge, the system was equipped with a filter to react only to objects flying at characteristic ATGM speeds. The four-barreled launchers were located on the forward part of the turret and only provided protection for the front 60? portion of the turret. To change the covered arc of coverage the crew would have to rotate the turret and orient the coverage cone on the threat.
T-55AD Drozd: Naval Infantry T-55A variant equipped with Drozd but not the Volna fire control system or ERA.
|
|
David
Sat January 3, 2004 10:20pm
Rating: 10
|
AK-47 Rifle
Function: All 7.62-mm Kalashnikov assault rifles are very dependable weapons. They produce a high volume of fire and are simple to maintain and produce.
Description: The "Avtomat Kalashnikova model 1947 g." or AK-47 is a gun designed by Mikhail Kalashnikov and produced by LZh, widely used by the USSR armed forces from the 1950s through the 1980s. It is classified as an assault rifle, a mid-caliber rifle (7.62 mm, which is approximately equal to .30 caliber) that can be fired semi-automatically, or in fully-automatic bursts. It is intentionally smaller and shorter-ranged than WWII battle rifles.
The AK47 was cheap, light to carry, and easy to clean and repair in the field. It was mostly reliable but the ejector pin sometimes broke. Derivative designs replaced the AK-47 during the 1980s.
It was favoured by non-Western powers because of its ease of use, robustness, and simplicity of manufacture. Copies were made by many factories in other countries including Israel, Finland, Hungary, China and Poland, where they remain in production today.
AK47 and AKM have been extensively modified and improved upon since their first designs. Standard Kalashnikovs include:
AK-47 1948-51, 7.62x39mm. The very earliest models had a stamped sheet metal receiver. Now rare.
AK-47 1952, 7.62x39mm: with a milled receiver and wooden buttstock and hand-guard. Barrel and chamber are chrome-plated to resist corrosion. Rifle weight 4.2Kg.
AKM 7.62x39mm: a revised, lower-cost version of the AK-47; receiver is precision-stamped sheet-metal. Rifle weight 3.61Kg.
AKS-74 5.45x39mm; note the new, much smaller ammunition.
AK-74M 5.45x39mm folding stock (for motorised infantry)
AKSU 5.45x39mm, tanker's self-defense weapon, folding stock, short barrel, altered sight and gas mechanism.
Later designations:
AK-101 5.56x45 mm round (NATO round)
AK-102 short stock 101
AK-103 7.62x39mm round
AK-104 short stock 103
AK-105 5.45x39mm round (short stock)
General Characteristics, AK-47 Rifle
Names:
AK, Kalashnikov
Date of Introduction:
1949/1961
Proliferation:
Widespread (over 50 million)
Weight (kg):
Loaded (with magazine): 3.8
Empty (w/o magazine): 4.3/3.14
Length (mm):
870/880
Rate of Fire (rounds/minute):
Cyclic: 600
Practical:
- Automatic: 100
- Semiautomatic: 40
Ceiling:
18,000 meters (59,055 feet)
Operation:
Gas
Feed:
30-round curved box magazine
Fire Mode:
Selective, automatic or semi-automatic
Sights:
INA
Type: Fore, pillar; rear, U-notch
Magnification: None
|
|
David
Sat January 3, 2004 11:51pm
|
Deep Drone 7200 Remotely
Function: Deep sea underwater recovery.
Description: The Deep Drone is a 7,200-foot depth rated Remotely Operated Vehicle (ROV). The system is designed to meet the Navy's needs for deep ocean recovery. The system is air transportable on military cargo aircraft and is designed to operate from various ships.
Features: The operator can control the ROV in all six degrees of freedom. Auto-control functions are provided for depth, altitude, and heading. The vehicle is capable of functioning with both long and short baseline bottom navigation systems. The vehicle uses electric propulsion, giving it a low noise signature. It carries a target locating sonar and has two manipulators capable of working with tools and attaching rigging. For photographic documentation, the vehicle has a 35mm still camera and both black and white and color television cameras that produce quality videotape. Electrical power for the system is provided by a diesel generator or the power system of the supporting ship if it is compatible. For special operations, the ROV can accommodate custom, skid-mounted tool packages. These packages could include, but are not limited to, trenchers, specialized salvage tools, and instrument packages or other mission-oriented equipment.
General Characteristics, Deep Drone 7200
Propulsion:
Electrical
Length, Overall:
9 feet 3 inches (2.8194 meters)
Width:
4 feet 7 inches (1.397 meters)
Displacement:
67.5 tons
Height:
6 feet 2 inches (1.8796 meters)
Lift Capacity:
3,200 pounds (1,451.52 kilograms)
Payload:
300 pounds (136.08 kilograms)
Maximum Operating Depth:
7,200 feet (2,194.56 meters)
Lift Capacity:
3,200 pounds (1,451.52 kilograms)
Speed:
3 knots (5.559 kmh)
|
|
David
Sun January 4, 2004 12:31am
|
AGSS 555 USS Dolphin Reas
Function: The USS Dolphin (AGSS 555) is the Navy's only operational, diesel-electric, deep-diving, research and development submarine.
History: Shortly after her commisioning in 1968, the USS Dolphin established an unmatched world depth record for operational submarines. The submarine has since amassed an impressive record of scientific and military accomplishments, and now serves as a unit of the U.S. Naval Submarine Force, U.S. Pacific Fleet, under Commander, Submarine Development Squadron Five. Dolphin is home ported in San Diego and berthed at NCCOSC RDTE Division (NRaD) Pier 160. Employed by both civilian and Navy activities, the research submarine is equipped with an extensive instrumentation suite that supports missions such as acoustic deep-water and littoral research, near-bottom and ocean surveys, weapons launches, sensor trials, and engineering evaluations.
Description: Because she was designed as a test platform, USS Dolphin can be modified both internally and externally to allow installation of up to 12 tons of special research and test equipment. The submarine has internal and external mounting points, multiple electronic hull connectors, and up to 10 equipment racks for project use.
General Characteristics, USS Dolphin
Builders:
Portsmouth Naval Shipyard
Power Plant:
Diesel/Electric; 2 GM 12-cylinder, 425 HP engines
Date Deployed:
August 17, 1968
Length, Overall:
165 feet (50.29 meters)
Beam:
8 feet (2.44 meters)
Displacement:
950 long tons (965.25 metric tons) full load
Diameter:
18 feet (5.49 meters)
Maximum Operating Depth:
3,000 feet (914.40 meters)
Crew:
5 officer, 46 enlisted, and up to 5 scientists
Armament:
None
|
|
David
Thu January 8, 2004 3:03pm
|
Twentieth Army Air Force
Worn from 26 May 1944 to 1 March 1955.
Some combat elements of this unit moved in the summer of 1944 from the United States to India where they carried out very heavy bombardment operations against targets in Japan, Formaosa, Thiland, and Burma. Other combeat elements began moving late in 1944 from the US to the Marianas, being jo8ined there early in 1945 by the elements that had been in India. From the Marianaas, the Twentieth bonducted a strategic air offensive that was climaxed by the dropping of two atomic bombs on Japan. This unit also served in combat for a short time at the beginning of the Korean War. Among the commanders of this air force were General of the Army, Henery H. "Hap" Arnold, Major General Curtis E. LeMay and Lietenant General Nathan F. Twining. The winged star represents the army air forces, and the arabic number twenty is the unit's designation. Both are superimposed upon a globe. Activated 4 April 1944 at Washington D.C.
Campaigns:
WWII (American thater; India-Burma; Air Offensive, Japan; China Defensive; Eastern Mandates; Western Pacific; Central Burma).
|
|
David
Thu January 8, 2004 3:03pm
|
Air Force Air Transport C
The Air Force Air Transport Command (AFATC) shoulder patch was changed from the design previously used by its parent unit the Air Force Ferrying Command. This modified patch would be of the same general design but would be silver, instead of gold, and the morse code would read "AFATC" instead of the "AFFC". The design of the shoulder patch suggests a stylized aircraft being ferried from east to west over a portion of the globe. The design is based on a Presidential Directive from Franklin D. Roosevelt (as Commander in Chief) ordering that ircraft be ferried for delivery to the British "with the greatest possible speed." It should be noted that the short and long red and blue lines extending from the globe to the tip of the wing form the Morse code letters and were part of the originally approved design. Although the QMG made no mention of the new "cloth" insignia just the metal insignia, it is believed that these patches were worn by local approval only.
The AFATC was established on June 20th, 1942, as a successor Command to the SAir Forces Ferrying Command with Headquarters in Washington, D.C. The Ferrying Division of AFATC took charge of all ferrying operations and continured this missiion of ferrying aircraft to foreign and domestic destinations and often delivered 8,000 aircraft monthly. AFATC was also made responsible for transporting all War Department personnel, material, and mail (escept for areas served by Troop Carrier Units). In addition, AFATC was given the control, operation, and maintenance for all air route facilities and establishments in effect, the AFATC became "an agency in which the War Department had centered a;ll responsibbility for the development of air transport." To accomplish its mission, AFATC established a network of over 200 bases along 100,000 miles of overseas routes and 35,000 miles of domestic routes. Aircraft from civilian carriers were contracted (Air Carrier Contracat Personnel)) and added to the Command, ad passenger service became a major function of AFATC. With the addition of overseas wings to the Command, the prompt delivery of cargo to combat areas in any theater of operations became "one of the most significant developments of the war." While statistics do not indicat4 how many battles were won by the prompt delivery of priority cargo to the battlefront by the Air Transport Command, history reveals that no battle was ever lost because of a lack of support from the men of this fine unit.
|
|
David
Thu January 8, 2004 3:22pm
|
Nineteenth Armored Divisi
Worn from 1 July 1946 to 20 August 1947
Tab: NONE
Activated at Los Angeles, California. The Arabic number nineteen shows the division's designation. The Sixteenth had no nickname since they were so short lived. The unit was redesignated as the 13th Armored Division because of the historical ties between California an the 13th Armored Division.
Campaigns: NONE
|
|
|
The Patriot Files Forums
