David
Sat January 18, 2003 9:52am
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A T-37 Tweet aircraft fro
A T-37 Tweet aircraft from the 85th Fighter Training Squadron, Laughlin AFB, Texas, flies over Lake Amistad during a training mission. The T-37 Tweet is a twin-engine jet used for training undergraduate pilots, undergraduate navigator and tactical navigator students in fundamentals of aircraft handling, and instrument, formation and night flying. The twin engines and flying characteristics of the T-37 give student pilots the feel for handling the larger, faster T-38 Talon or T-1A Jayhawk later in the undergraduate pilot training course. The instructor and student sit side by side for more effective training. The cockpit has dual controls, ejection seats and a clamshell-type canopy that can be jettisoned.
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David
Sat January 18, 2003 9:52am
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A T-37 Tweet aircraft fro
A T-37 Tweet aircraft from the 85th Fighter Training Squadron, Laughlin AFB, Texas, flies over Lake Amistad during a training mission. The T-37 Tweet is a twin-engine jet used for training undergraduate pilots, undergraduate navigator and tactical navigator students in fundamentals of aircraft handling, and instrument, formation and night flying. The twin engines and flying characteristics of the T-37 give student pilots the feel for handling the larger, faster T-38 Talon or T-1A Jayhawk later in the undergraduate pilot training course. The instructor and student sit side by side for more effective training. The cockpit has dual controls, ejection seats and a clamshell-type canopy that can be jettisoned.
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David
Sat January 18, 2003 9:52am
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The T-38 Talon is a twin-
The T-38 Talon is a twin-engine, high-altitude, supersonic jet trainer used in a variety of roles because of its design, economy of operations, ease of maintenance, high performance and exceptional safety record. It is used primarily by Air Education and Training Command for undergraduate pilot and pilot instructor training. Air Combat Command, Air Mobility Command and the National Aeronautics and Space Administration also use the T-38 in various roles.
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David
Sat January 18, 2003 9:52am
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T-38 Talons in a four-shi
T-38 Talons in a four-ship formation are twin-engine, high-altitude, supersonic jet trainers used by the 50th Fighter Training Squadron, Columbus AFB, Miss. in a variety of roles because of its design, economy of operations, ease of maintenance, high performance and exceptional safety record. Primarily Air Education and Training Command uses it for undergraduate pilot and pilot instructor training. Student pilots fly the T-38A to learn supersonic techniques, aerobatics, formation, night and instrument flying and cross-country navigation. More than 60,000 pilots have earned their wings in the T-38A. Air Education and Training Command uses a modified version, the AT-38B, to prepare pilots for fighter aircraft such as the F-15, F-16, A-10 and F-111. This model carries external armament and weapons delivery equipment for training.
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David
Sat January 18, 2003 9:52am
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A T-37 Tweet aircraft fro
A T-37 Tweet aircraft from the 85th Fighter Training Squadron, Laughlin AFB, Texas, flies over Lake Amistad during a training mission. The T-37 Tweet is a twin-engine jet used for training undergraduate pilots, undergraduate navigator and tactical navigator students in fundamentals of aircraft handling, and instrument, formation and night flying. The twin engines and flying characteristics of the T-37 give student pilots the feel for handling the larger, faster T-38 Talon or T-1A Jayhawk later in the undergraduate pilot training course. The instructor and student sit side by side for more effective training. The cockpit has dual controls, ejection seats and a clamshell-type canopy that can be jettisoned.
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David
Sat January 18, 2003 12:28pm
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An A-10 Thunderbolt II fr
An A-10 Thunderbolt II from the 81st Fighter Squadron, Spangdahlem Air Base, Germany, takes off on a mission against targets in Yugoslavia, April 5, 1999. Members of the 81st Fighter Squadron are deployed to Aviano Air Base, Italy, in support of NATO Operation Allied Force. The A-10 and OA-10 Thunderbolt IIs are the first Air Force aircraft specially designed for close air support of ground forces. They are simple, effective and survivable twin-engine jet aircraft that can be used against all ground targets, including tanks and other armored vehicles.
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David
Sat January 18, 2003 12:40pm
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HH-60 Pave Hawk helicopte
HH-60 Pave Hawk helicopters. The Pave Hawk is a twin-engine medium-lift helicopter operated by the Air Force Special Operations Command, a component of the U.S. Special Operations Command. During Desert Storm, Pave Hawks provided combat recovery for coalition air forces in Iraq, Saudi Arabia, Kuwait and the Persian Gulf. They also provided emergency evacuation coverage for U.S. Navy sea, air and land (SEAL) teams penetrating the Kuwait coast before the invasion.
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David
Tue February 4, 2003 8:19am
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David
Tue February 4, 2003 8:19am
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David
Sat January 3, 2004 9:38pm
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An-124 Condor
Function: High payload, long range cargo aircraft.
History: Introduced in 1982 as a long range, heavy lift cargo and troop transport aircraft, the Antonov An-124 Ruslan (NATO designation Condor) is currently the world's largest and heaviest payload aircraft in production in the world. Outclassing the C-5 Galaxy by nearly 20 tons in payload capacity, and the Ilyushin Il-76 by more than 100 tons, the An-124 is only exceeded in lifting ability by the special purpose An-225 Mriya (NATO designation Cossack) which was purpose built to transport the Russian space shuttle, and of which only two were built.
Currently in production at the AVIASTAR facility in Ulyanovsk and the AVIANT State Aviation Plant in Kiev, the An-124, in addition to serving with the Russian military as a long range high payload cargo aircraft capable of delivering or airdropping troops, and equipment, is also in service with a number of civilian organizations as a dedicated cargo transport. Antonov Airlines, Volga-Dniepr, and Poliot all employ the An-124, using it to transport heavy and over sized equipment such as hydraulic turbines, mobile cranes, railway locomotives, earthmovers and dump trucks, and sailing vessels. The An-124 is even capable of transporting other aircraft, ferrying partially disassembled passenger planes to customers worldwide.
To facilitate the loading and unloading of cargo, the nose section is hinged to open upwards, and the tail section is fitted with a pair of clamshell doors. Both nose and tail sections are equipped with integral loading ramps. In addition, the An-124 also employs two traveling cranes, two winches, a rollgang and tie down equipment which limit it's dependence on ground equipment for cargo handling and manipulation. The Ruslan is equipped with multi leg, self-orienting landing gear and is rough surface capable. The landing gear height can be adjusted on the ground, to facilitate loading cargo.
In addition to the An-124-100 currently in production, Air Foyle (UK) in conjunction with Antonov and Aviastar has proposed the construction of two new versions, the An-124-210, and the An-124-100M. Both versions will be equipped with Western and Russian digital instruments and displays which will reduce the crew size from 6 to 4. In addition, both will be equipped with a traffic alert collision and avoidance system, ground proximity warning system and a satellite communications system. The 210 will be outfitted with Rolls-Royce RB211-52H-T engines, while the 100M will be equipped with the Series 3 D-18 engines, produced by the Progress Design Bureau in Zaporozhe. Each of these engine upgrades will increase the Ruslan's range by 10% and reduce take off distance.
Description: Typical of most cargo aircraft, the An-124 body forms a thick oval cross-section, with a tapered aft section and rounded nose to facilitate cargo handling. The fuselage is of a twin deck design, the upper deck being the flight deck, and the lower deck serving as the cargo hold. On the flight deck are the cockpit, with stations for the six crewmembers, a relief crew compartment, and seating for an additional 88 passengers. The loadmaster's station is on the cargo deck.
The wings are mounted high on the fuselage at a negative dihedral, are tapered and swept, with a relatively high cross-section to increase efficiency and range. The four Lotarev D-18T turbofans are mounted on pylons underneath the wings. The horizontal stabilizers are also swept back and tapered, and are mounted at mid level on the fuselage, aft of the vertical stabilizer.
General Characteristics, AN-124 Condor
Power Plant:
Four D-18T turbofans (An-124-100)
Four D-18T Series 3 (An-124-100M)
Four RB211-524H-T (An-124-210)
Thrust:
229 kN (153,558 pounds)
An-124-210: 264 kN (177,027 pounds)
Length:
69.1 meters (226.4 feet)
Height:
21.08 meters (69.2 feet)
Wingspan:
73.3 meters (240.5 feet)
Cargo Hold Dimensions:
Floor length including ramps: 36.5 meters
Width at floor level: 6.4 meters
Height: 4.4 meters
Volume cargo hold: 1,270 cubic meters
Speed:
800 to 850 kmh
Cruise speed at an altitude of 9 km: 750 to 800 kmh
Ceiling:
12,000 meters (39,370 feet)
Load-Carrying Capacity:
120 tons using a 2,800 meter runway (2300 meters for An-124-210)
150 tons using a 3,000 meter runway (2500 meters for An-124-210)
Maximum Takeoff Weight:
392 tons
Range:
With maximum fuel: 13,300 kilometers (7,980 miles) (15,250 for An-124-210)
With 40-ton payload: 10,960 kilometers (6,576 miles) (12,730 for An-124-210)
With 120-ton payload: 5,030 kilometers (3,018 miles) (5,950 for An-124-210)
Crew:
Seven (An 124)
Four (An-124-100)
Four (An-124-100M)
Three (An-124-210)
Runway:
3000 meters (2,420 for An-124-210)
Takeoff run on concrete runway: 2520 meters (2,420 for An-124-210)
Landing roll on concrete runway: 900 meters
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David
Sat January 3, 2004 9:38pm
Rating: 10
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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
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David
Sat January 3, 2004 9:38pm
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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
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David
Sat January 3, 2004 10:15pm
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BTR-70 APC
Function: Soviet 1970-era wheeled APC.
Background: Introduced in 1978 as a replacement to the BTR-60, The BTR-70 is very similar externally to the older vehicle, as many if the improvements made to the vehicle are internal.
The BTR-70 uses the standard Warsaw Pact APC weapons turret equipped with one KPV 14.5mm machine gun and one PKT 7.62mm machine gun. As with the BTR-60, power is supplied to all eight wheels by means of a unique twin engine/transmission arrangement. The BTR-70's power plants, however, have been upgraded to two 120hp gasoline engines. The gearbox arrangement, however, remains unchanged; one supplies power to the 1st and 3rd axles and the other supplies power to the 2nd and 4th axles.
The BTR-70 is also fully amphibious and does not require any preparation time. Steering, both on land and in the water, is provided by the forward two axles, which are also power assisted. Water propulsion is provided by a single rear mounted water jet.
Though replaced by the BTR-80 in the early eighties, the BTR-70 continues to serve in many armies world-wide, including most former Warsaw Pact as well as many Middle Eastern, African, and Asian countries.
Description: The BTR-70 an all-wheeled 8x8 fully amphibious armored personnel carrier. The boat shaped vehicle is divided up into three sections: crew compartment, personnel compartment, and engine compartment. In the case of the BTR-70 the hull has been lengthened somewhat and the axles now have a paired appearance, with a distinctive gap between the second and third axles.
The BTR-70 may be readily distinguished from the 60 and 80 series by the presence of a single, large, curved "caterpillar" insulated exhaust located on either side of the hull rear. In addition the amphibious operations trim vane has been moved from underneath the nose of the vehicle, BTR-60 series, to on top of the nose, just forward of the driver's station.
The BTR-70 is equipped with the standard Warsaw Pact APC turret. The small, one man turret is mounted over the second axle and contains one KPV 14.5mm machine gun and one PKT 7.62mm machine gun.
The personnel compartment can be accessed by a triangular doorway located between the second and third axles. The three infantry mounting steps and the three additional mounting rails located on the hull above the steps, present on the BTR-60, have been eleminated. The large personnel compartment access hatches located on each side of the hull have also been eliminated and replaced with three firing ports.
General Characteristics, BTR-70 Armored Personnel Carrier
Manufacturers:
Soviet Union
Transmission:
2x manual
Engine:
2x 120hp V-8 gasoline
Length:
25.51 feet (7.85 meters)
Width:
9.1 feet (2.80 meters)
Height:
7.96 feet (2.45 meters)
Combat Weight:
11.5 tons
Cruising Range:
450 kilometers
Speed:
Maximum: 50mph ( 80kph)
Off-road: 38mph (60kph)
Fording:
Fully amphibious without preparation
Crew:
2; driver, gunner-commander
8 passengers
Armament:
Main:
One 14.5mm KPV HMG
Secondary:
One 7.62mm PKT-T MG
Introduction Date:
1978
Variants:
BTR-70 M1986/1: Improved version of the Basic BTR-70.
BTR-70Kh: Chemical recon variant. Equipped with a proximity fuse jammer. This device is designed to prematurely detonate proximity fused artillery rounds.
BTR-70MS: Communications support variant.
BTR-70KShM: Mobile command post variant.
BREM: Armored Recovery Vehicle variant.
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David
Sat January 3, 2004 10:15pm
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BTR-60 APC
Function: Soviet 1950 era wheeled APC.
Background: Introduced in 1963 as a replacement for the fully tracked BTR-50, the BTR-60 represents the first of a series of 8x8 wheeled APC that are still in production in the former Soviet Union. In terms of numbers produced, the BTR-60 was the most important vehicle in the Soviet Army and was issued to the Soviet naval Infantry. In addition, the BTR-60 has been supplied to most Warsaw Pact countries in addition to North Korea. The BTR-60 has also been manufactured in Czechoslovakia and Poland.
Initial BTR-60s were equipped with a single 12.7mm DShK machine gun and two PKT 7.62mm machineguns, all mounted forward of the personnel compartment. Later models used the standard Warsaw Pact APC weapons turret equipped with one KPV 14.5mm machine gun and one PKT 7.62mm machine gun. Power is supplied to all eight wheels by means of a unique twin engine/transmission arrangement. The BTR-60 uses two V-8 90hp gasoline engines and two separate transmissions; one supplies power to the 1st and 3rd axles and the other supplies power to the 2nd and 4th axles.
The BTR-60 is fully amphibious and does not require any preparation time. Steering, both on land and in the water, is provided by the forward two axles, which are also power assisted. Water propulsion is provided by a single rear mounted water jet.
Although the BTR-70 began to replace the BTR-60 in 1978, the BTR-60 has never been retired, and continues to serve in Russian reserve formations and numerous countries world-wide.
Description: The BTR-60 an all-wheeled 8x8 fully amphibious armored personnel carrier. The boat shaped vehicle is divided up into three sections: crew compartment, personnel compartment, and engine compartment. In early versions the personnel compartment is open topped; in later versions the entire vehicle is fully enclosed. The BTR-60 may be readily distinguished from the later 70/80/90 series by the presence of a single "automotive-type" muffler exhaust located on either side of the hull rear.
The BTR-60 "P" and "PA" variants are equipped with a single 12.7mm DShK machine gun and two PKT 7.62mm machineguns. These MGs are mounted forward of the personnel compartment, and require the gunners to be exposed while firing. Because of the size of the gunner's position, only two of the three MGs can be manned at any given time. The "PB" model is equipped with a small, one man, turret, mounted over the second axle that contains one KPV 14.5mm machine gun and one PKT 7.62mm machine gun.
In all models, the personnel compartment can only be accessed from the roof of the carrier. There are three infantry mounting steps on each side of the vehicle, mounted between the road wheels, and three additional mounting rails located on the hull above the steps. There is a large personnel compartment access hatch located on each side of the hull.
General Characteristics, BTR-60 Armored Personnel Carrier
Manufacturers:
Soviet Union, Czechoslovakia, and Poland.
Transmission:
2x manual
Engine:
2x 90hp V-8 gasoline
Length:
23.47 feet (7.22 meters)
Width:
9.17 feet (2.82 meters)
Height:
6.7 feet (2.06 meters)
Combat Weight:
10.1 tons
Cruising Range:
500 kilometers
Speed:
Maximum: 50mph ( 80kph)
Off-road: 38mph (60kph)
Fording:
Fully amphibious without preparation
Crew:
Two (driver, gunner-commander)
12 passengers
Armament:
Main:
One 12.7mm DShK HMG (BTR-60P)
One 14.5mm KPV HMG (BTR-60PB)
Secondary:
Two7.62mm PKT-T MG (BTR-60P)
One 7.62mm PKT-T MG (BTR-60PB)
Introduction Date:
1961
Variants:
BTR-60P: Initial production model. The BTR-60P was open topped and armed with a single 12.7mm DShK machine gun.
BTR-60PA: Modified "P" model. Incorporates overhead cover for the personnel compartment. Because of space restrictions in the gunner's hatch, no more than two of the weapons can be manned at any given time.
BTR-60PB: Most widely fielded varient. Has increased overhead protection for passengers and crew and incorporates the standard Warsaw Pact APC weapons turret. This one-man turret houses one KPV 14.5mm machine gun and one PKT 7.62mm machine gun.
BTR-60PBK: Command variant with additional communications equipment.
BTR-60 PU: Armored command vehicle (ACV) variant for battalion level. The "PU" is open-topped and can be identified by its canvas roof, additional communication equipment and lack of weapons turret. The "PU" also has an easily recognizable dipole antenna that runs nearly all around the top of the vehicle.
BTR-60 PU-12 and -12M: "U" and "PU" variants used by air defense controllers and configured for ground to air communication.
BTR-60 R-975: Forward Air Control Vehicle (FACV). A modified BTR-60PB with sighting optics and laser designator installed in the turret in place of the weapons. Can also be identified by the large portable generator mounted on the rear of the vehicle.
MTP-2: Armored recovery vehicle.
R-145BM: ACV used ad Brigade level. Has increased radio range and communications capabilities.
ACRV 1V18: Artillery command and reconnaissance vehicle. The 1V18 is a command and observation vehicle (COP) while the 1V19 variant serves as an artillery fire direction center (FDC).
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David
Sat January 3, 2004 10:24pm
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Victor III Class Nuclear
Function: Nuclear powered attack submarine.
History: The Project 671RTM class (NATO Victor III) nuclear attack submarine (SSN) was designed based off of information delivered to the Soviet Union via the Walker spy ring. The documents delivered by the Walker family compromised every aspect of the American navy's antisubmarine warfare program. What these documents revealed was just how badly outclassed the Soviets were in submarine warfare. The current Soviet production submarines, the Pr. 671RT, were shown to be so noisy that not only was the US Navy able to maintain a "real time" position fix on these submarines, but that their own noise levels defeated the effectiveness of their own offensive sensors. In effect, had war between the Soviet Union and the United States been initiated, the Soviet submarine fleet would have been decimated.
The information provided by the Walker spies changed all this. Following their disclosures, the Soviet navy initiated a crash program to quiet its current fleet of submarines as well as improve their offensive capabilities, which were still based on World War Two technology. Designated the Pr. 671RTM, this new series would incorporate rafted and insulated machinery, a brand new sonar suite which emphasized passive detection capabilities as well as new twin flank arrays and a new towed sonar array. Improvements would be made in the processing of this additional sonar information, culminating with the development of an integrated combat system for the Pr. 671RTMK series (this was made possible through the acquisition of a Norwegian navy software program and Toshiba computer components). Externally similar to the Pr. 671RTM, the 671RTMK incorporates, among other improvements, the non acoustic sensor complex built for the Pr. 971 boats. The 671RTM/RTMK hulls were armed with four bow mounted 53cm torpedo tubes and four bow mounted 65cm torpedo tubes. Unlike the Pr. 685 submarines, the Barrakuda had a large torpedo room with a capacity for 40 weapons, including 53 and 65cm wake following and wire guided torpedoes, BA-111 Shkval underwater rockets, P-100 anti-ship missiles, RPK-6 rocket delivered nuclear depth charges, and RPK-7 rocket delivered homing torpedoes.
Deployed roughly at the same time as the American Improved Los Angeles class fast attack submarines, the 671RTM boats were comparable with the much earlier Permit class American Submarines while the 671RTMK were the equivalent to the later Sturgeon class in terms of performance. Production was stopped at 26 submarines with 14 still in limited service. The remaining 671RTM series submarines will be withdrawn from service once their reactor life has been exhausted.
General Characteristics, K.138 (Victor III) Class
Builders:
Krasnoye Soromovo Zavod 112, Nizhniy Novgorod
Power Plant:
Two VM-4T rated at 72 Megawatts each, two steam turbines, one shaft with one VRSh-7 controllable pitch screw or two VRSh-4 screws on a single shaft, 31,000 shaft horsepower
Length, Overall:
351.6 feet (107.2 meters)
Beam:
35.4 feet (10.8 meters)
Draft:
24.2 feet (7.4 meters)
Displacement:
6,990 tons submerged
Speed:
30 knots submerged
Crew:
27 Officers; 73 Enlisted
Maximum Safe Diving Depth:
1,150 feet
Armament:
Four bow mounted 53cm torpedo tubes
Two bow mounted 65cm torpedo tubes
P-100 Oniks (NATO SS-N-22 SUNBURN) anti-ship missiles
Two RPK-2 Viyoga (NATO SS-N-16 STARFISH) rocket delivered nuclear depth charges or two S-10 Granet (NATO SS-N-21 SAMPSON) strategic cruise missiles
Six RPK-7 Vodopei (NATO SS-N-16 STALLION) rocket delivered homing torpedoes (ASW variant)
Six P-100 Oniks (NATO SS-N-22 SUNBURN) anti-ship missiles (ASuW variant)
BA-111 Shkval underwater rockets
Type 53-65K torpedoes
SET-65 torpedoes
TEST-68 wire guided torpedoes
Sensors:
Vodopod combat direction system (671RTM)
Viking combat direction system (671RTMK)
Radar:
One MRK-50 Topol surface search radar
One Medvyedista-671 navigation radar
Sonar:
One MGK-400 Rubikon active/passive sonar suite
Two Akula flank arrays One Pithon towed array
One MG-24 Luch mine detection sonar
Countermeasures:
Bulava ESM/ECM system
Two MG-74 Korund noise simulation decoys
One MT-70 sonar intercept receiver
Nikhrom-M IFF system
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