Showing posts with label lockheed. Show all posts
Showing posts with label lockheed. Show all posts

Wednesday, May 3, 2017

Lockheed Martin F 35 Lightning II

Lockheed Martin F 35 Lightning II



The Lockheed Martin F-35 Lightning II is scheduled to be introduced in 2011. It was a descendant of the X-35, which was the product of the Joint Strike Fighter Program (J.S.F.). Once operational, it will replace the U.S.M.C.s McDonnel Douglas AV-8B Harrier II. The reason is the F-35 is capable of V/STOL, which stands for Vertical/Short Take-off and Landing. In addition to that, the F-35 is capable of stealth, which is a very valuable capability.

Although not operational yet, the F-35 is already being planned for exports to countries from the United Kingdom to Singapore.

Design...

The F-35 appears to be a smaller, slightly more conventional, one-engine sibling of the sleeker, two-engine F-22 Raptor, and indeed, drew elements from it. The exhaust duct design was inspired by the General Dynamics Model 200, a 1972 VTOL aircraft designed for the Sea Control Ship.

Lockheed teamed with the Yakovlev Design Bureau, developer of the Yakovlev Yak-141 "Freestyle", in the 1990s.

Stealth technology makes the aircraft hard to detect as it approaches short-range tracking radar.

Some improvements over current-generation fighter aircraft are:

  • Durable, low-maintenance stealth technology;
  • Integrated avionics and sensor fusion that combine information from off- and onboard sensors to increase the pilots situational awareness and improve identification and weapon delivery, and to relay information quickly to other command and control (C2) nodes;
  • High speed data networking including IEEE-1394b and Fibre Channel.
  • Low life-cycle costs.

Operational History...

Although the F-35 has not experienced any combat as it is not operational yet, it has been thorugh extensive testing and is still under developemnt.

Testing...

  • On 19 February 2006, the first F-35A (USAF version) was rolled out in Fort Worth, Texas. The aircraft underwent extensive ground testing at Naval Air Station Fort Worth Joint Reserve Base in fall 2006. On 15 September 2006 the first engine run of the F135 afterburning turbofan was conducted in an airframe, with the tests completed on 18 September after a static run with full afterburner. The engine runs were the first time that the F-35 was completely functional on its own power systems. On 15 December 2006, the F-35 completed its maiden flight.
  • On 3 May 2007, an electrical problem consisting of electrical arcing inside a hydraulic control box forced the aircraft to make an emergency landing. It was grounded until 7 December, when test pilot Jon Beesley flew a 55-minute test flight.
A unique feature of the test program is the use of the so-called Lockheed CATBird avionic testbed, a highly modified Boeing 737-330, inside of which are racks holding all of F-35s avionics, as well as a complete F-35 cockpit.
  • On 31 January 2008 at Fort Worth, Texas, Lt. Col. James "Flipper" Kromberg of the U.S. Air Force became the first military service pilot to evaluate the F-35, taking the aircraft through a series of maneuvers on its 26th flight.
  • On 12 March 2008, the first F-35A (AA-1) began aerial refueling testing on its 34th test flight.

Variants...

  • F-35A Conventional Takeoff and Landing (CTOL)

Intended for the USAF and other air forces, the F-35A is the smallest, lightest, and most agile variant. It is also the only one equipped with an internal cannon (GAU-22/A). It is expected that the F-35A will match and outperform the F-16 in almost all expects and is intended for replacing the Fighting Falcon (F-16).

  • F-35B Short Takeoff and Vertical Landing (STOVL)

Intended for the USMC, the F-35B sacrifices some fuel volume for its vertical takeoff system. It is also less maneuverable than the A variant, being stressed to 7 gs instead of the 9 for the F-35A. Since the F-35B has a vertical landing system, it does not have a landing hook. This aircraft will replace all F/A-18 Hornets and the attack and fighter roles of the AV-8B Harrier II, in the Marine Corp inventory.

  • F-35C Carrier Variant

The F-35C features a lager wing that has the ability to fold (save space on aircraft carrier). This larger surface area for the wing will improve low speed control and decreases speed for landings while also increasing range and payload.The F-35C also has a strong landing gear for the stresses of carrier landings and a landing hook for carrier arrestor cables. The F-35C is intended to replace all F/A-18 Hornets A/B/C/D and serve as a low observable complement to th F/A-18E/F Super Hornet.

  • F-35I Israeli variant

The F-35I is an F-35A with Israeli modifications. Since this is so, the letter designation is I (for Israel).

Specifications...

Data from Lockheed Martin specifications (1, 2, 3) , F-35 Program brief, F-35 JSF Statistics (Download)

General Characteristics
  • Crew: 1
  • Length: 50 ft 6 in (15.37 m)
  • Wingspan: 35 ft 0 in (10.65 m)
  • Height: 17 ft 4 in (5.28 m)
  • Wing area: 459.6 ft² (42.7 m²)
  • Empty weight: A; 29,036 lb B; 32,161 lb C; 32,070 lb (13,170 kg A; 14,588 kg B; 14547 kg C;)
  • Loaded weight: 44,400 lb (20,100 kg)
  • Max takeoff weight: 60,000 lb (27,200 kg)
  • Powerplant: 1× Pratt & Whitney F135 afterburning turbofan
  • Dry thrust: 25,000 lbf (111 kN)
  • Thrust with afterburner: 40,000+ lbf (178+ kN)
  • Secondary Powerplant: 1× General Electric/Rolls-Royce F136 afterburning turbofan, >40,000 lbf (178 kN) [in development]
  • Lift fan (STOVL): 1× Rolls-Royce Lift System driven from either F135 or F136 power plant, 18,000 lbf (80 kN)
  • Internal fuel: F-35A: 18,480 lb (8,382 kg); F-35B: 14,003 lb (6,352 kg); F-35C: 20,085 lb (9,110 kg)
Performance
  • Maximum speed: Mach 1.6+ (1,200 mph, 1,931 km/h)
  • Range: A: 1,200 nmi; B: 900 nmi; C: 1400 nmi (A: 2,200 km; B: 1,667 km; C: 2,593 km) on internal fuel
  • Combat radius: 600 nmi (690 mi, 1,110 km)
  • Rate of climb: classified (not publicly available)
  • Wing loading: 91.4 lb/ft² (446 kg/m²)
  • Thrust/weight:
  • With full fuel: A: 0.89; B: 0.92; C: 0.81
  • With 50% fuel: A: 1.12; B: 1.10; C: 1.01
  • g-Limits
  • F-35A: 9 g
  • F-35B: 9 g
  • F-35C: 9 g
Armament
  • Guns: 1 × GAU-22/A 25 mm cannon — slated to be mounted internally with 180 rounds in the F-35A and fitted as an external pod with 220 rounds in the F-35B and F-35C.
  • Hardpoints: 6 with a capacity of 15,000 lb (6,800 kg),
  • Missiles: Internal: 2 air-air missiles and 2 air-surface weapons; External: 2 missiles and 4 missiles/bombs.

Available link for download

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Saturday, March 18, 2017

Lockheed Martin F 35 Lightning II Brief Description

Lockheed Martin F 35 Lightning II Brief Description


The latest and one of the most advanced aircraft in the world, the Joint Strike Fighter has not even been introduced, which is scheduled for 2011. Capable of stealth and V/STOL (Vertical of Short Take-off and Landing), the F-35 is a must-have for airforces that want air superioty.

Click here to read the full article

F-35 Lightning II.

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Saturday, March 4, 2017

Lockheed Martin Boeing F 22 Raptor

Lockheed Martin Boeing F 22 Raptor


An F-22 Raptor dropping flares

The F-22 Raptor is an American air superiority fighter that uses stealth technology. It is considered by the United States Air Force as a critical component of the United States Strike Force. In addition, the F-22 has multiple capabilities that include ground atack, electronics warfare, and signal intelligence roles.

It is claimed by many to be the worlds most effective air superiority fighter and it cannot be matched by any known or projected fighter aircraft. It is also said to be "most outstanding fighter plane ever built", as claimed by Air Chief Marshal Angus Houston, Chief of the Australian Defence Force in 2004.

Development...

In 1981 the United States Air Force (USAF) developed a requirement for a new air superiority fighter, the Advanced Tactical Fighter (ATF), to replace the capability of the F-15 Eagle. ATF was a demonstration and validation program undertaken by the USAF to develop a next-generation air superiority fighter to counter emerging worldwide threats, including development and proliferation of Soviet-era Su-27 "Flanker"-class fighter aircraft. It was envisaged that the ATF would incorporate emerging technologies including advanced alloys and composite materials, advanced fly-by-wire flight control systems, higher power propulsion systems, and low-observable/stealth technology.

A request for proposal (RFP) was issued in July 1986, and two contractor teams, Lockheed/Boeing/General Dynamics and Northrop/McDonnell Douglas were selected in October 1986 to undertake a 50-month demonstration/validation phase, culminating in the flight test of two prototypes, the YF-22 and the YF-23.

On 23 April, 1991 the USAF ended the design and test-flight competition by announcing Lockheeds YF-22 as the winner. It was anticipated at the time that 650 aircraft would be ordered.

Into production...

The first production F-22 was delivered to Nellis Air Force Base, Nevada, on 14 January, 2003 and "Dedicated Initial Operational Test and Evaluation" commenced on 27 October, 2004. By 2004, 51 Raptors were in service.

The first crash of a production F-22 occurred during take-off at Nellis Air Force Base on 20 December, 2004, in which the pilot ejected safely prior to impact. The crash investigation revealed that a brief interruption in power during an engine shutdown prior to flight caused a malfunction in the flight-control system; consequently, the technical data for the aircraft has been amended to avoid a recurrence of this problem.

In August 2007, the United States Air Force signed a $5 billion, multi-year contract with Lockheed Martin that will extend production to 2011, and as of 2008, F-22 Raptors are being procured at the rate of 20 per year.

In a ceremony on 29 August, 2007, Lockheed Martin reached its "100th F-22 Raptor" milestone, delivering aircraft 05-4100.

Proposed foreign purchases...

Unlike many other tactical fighters, the opportunity for export is currently non-existent because the export sale of the F-22 is barred by federal law. There was a time in the 1970s when the then-new F-16 was similarly restricted. However, regardless of restrictions, very few allies would even be considered for export sale because the F-22 is such a sensitive and expensive system. Most current customers for U.S. fighters are either acquiring earlier designs like the F-15 or F-16, or else are waiting to acquire the F-35, which contains much of the F-22s technology but is designed to be cheaper and more flexible.

The Japanese government reportedly showed some interest in buying F-22As in its Replacement-Fighter program for its Air Self-Defense Force (JASDF). In such an event, it would most likely involve a "watered-down" export variant while still retaining most of its advanced avionics and stealth characteristics. However, such a proposal would still need approval from the Pentagon, State Department and Congress.

Israeli Air Force (IAF) chief procurement officer Brigadier-General Zeev Snir said that, "The IAF would be happy to equip itself with 24 F-22s, but the problem at this time is the US refusal to sell the aircraft, and its $200 million price tag."

Some Australian politicians and defense commentators have proposed that Australia purchase F-22s instead of the F-35. In 2006, the Australian Labor Party supported this proposal on the grounds that the F-22 is a proven, highly capable aircraft, while the F-35 is still under development. However, the Howard government ruled out purchase of the F-22, on the grounds that it is unlikely to be released for export, and does not have sufficient ground/maritime strike capacity. This assessment was supported by the Australian Strategic Policy Institute, which claimed that the F-22 "has insufficient multi-role capability at too high a price." The ASPI analysis was, however, criticized by Air Power Australia.

The US Congress upheld the ban on F-22 Raptor foreign sales during a joint conference on September 27th, 2006. After talks in Washington in December 2006, the US DoD reported the F-22 would not be available for foreign sale.

Following the victory of the Australian Labor Party in the 2007 national election, the new government ordered a review of plans to procure the F-35 and F/A-18E/F Super Hornet. This review will include an evaluation of the F-22s suitability for Australia; moreover, Defence Minister Joel Fitzgibbon has stated: "I intend to pursue American politicians for access to the Raptor". In February 2008, U.S. Defense Secretary Robert Gates said he had no objection to sale of the Raptor to Australia, but Congress would have to change the law.

Characteristics...

The F-22 is a fifth-generation fighter that is considered a fourth-generation stealth aircraft by the USAF. Its dual afterburning Pratt & Whitney F119-PW-100 turbofans incorporate thrust vectoring, but in the pitch axis only, with a range of ±20 degrees. The maximum thrust is classified, though most sources place it at about 35,000 lbf (156 kN) per engine. Maximum speed, without external weapons, is estimated to be Mach 1.72 in supercruise mode; as demonstrated by General John P. Jumper, former US Air Force Chief of Staff, when his Raptor exceeded Mach 1.7 without afterburners on 13 January, 2005. With afterburners, it is "greater than Mach 2.0" (1,317 mph, 2,120 km/h), according to Lockheed Martin; however, the Raptor can easily exceed its design speed limits, particularly at low altitudes, with max-speed alerts to help prevent the pilot from exceeding them. Former Lockheed Raptor chief test pilot Paul Metz stated that the Raptor has a fixed inlet; but while the absence of variable intake ramps may theoretically make speeds greater than Mach 2.0 unreachable, there is no evidence to prove this. Such ramps would be used to prevent engine surge resulting in a compression stall, but the intake itself may be designed to prevent this. Metz has also stated that the F-22 has a top speed greater than 1,600 mph (Mach 2.42) and its climb rate is faster than the F-15 Eagle due to advances in engine technology, despite the F-15s thrust-to-weight ratio of about 1.2:1, with the F-22 having a ratio closer to 1:1. The US Air Force claims that the F-22A cannot be matched by any known or projected fighter.

Airframe...

Several small design changes were made from the YF-22A prototype to the production F-22A. The swept-back angle on the wings leading edge was decreased from 48 degrees to 42 degrees, while the vertical stabilizer area was decreased 20%. To improve pilot visibility, the canopy was moved forward 7 inches (178 mm) and the engine intakes were moved rearward 14 inches (356 mm). The shape of the wing and stabilator trailing edges was refined to improve aerodynamics, strength, and stealth characteristics.

Stealth...

Although several recent Western fighter aircraft are less detectable on radar than previous designs using techniques such as radar absorbent material-coated S-shaped intake ducts that shield the compressor fan from reflecting radar waves, the F-22 design placed a much higher degree of importance on low observance throughout the entire spectrum of sensors including radar signature, visual, infrared, acoustic, and radio frequency.

The stealth of the F-22 is due to a combination of factors, including the overall shape of the aircraft, the use of radar absorbent material (RAM), and attention to detail such as hinges and pilot helmets that could provide a radar return. However, reduced radar cross section is only one of five facets that designers addressed to create a stealth design in the F-22. The F-22 has also been designed to disguise its infrared emissions to make it harder to detect by infrared homing ("heat seeking") surface-to-air or air-to-air missiles. Designers also made the aircraft less visible to the naked eye, and controlled radio and noise emissions. The Raptor has an under bay carrier made for hiding heat from missile threats, like surface-to-air missiles.

The F-22 apparently relies less on maintenance-intensive radar absorbent material and coatings than previous stealth designs like the F-117. These materials caused deployment problems due to their susceptibility to adverse weather conditions. Unlike the B-2, which requires climate-controlled hangers, the F-22 can undergo repairs on the flight line or in a normal hangar. Furthermore, the F-22 has a warning system (called "Signature Assessment System" or "SAS") which presents warning indicators when routine wear-and-tear have degraded the aircrafts radar signature to the point of requiring more substantial repairs. The exact radar cross section of the F-22 remains classified.

Operational History...

Intended to be the leading American advanced tactical fighter in the early part of the 21st century, the Raptor is an expensive fighter with an incremental cost of about US$138 million per unit. The number of aircraft to be built has dropped to 183, down from the initial requirement of 750. Part of the reason for the decrease in the requirement is that the F-35 Lightning II uses much of the technology used on the F-22, but at a much more affordable price. To a large extent the cost of these technologies is only lower for the F-35 because they have already been developed for the F-22.

YF-22 "Lightning II"...

The prototype YF-22 won a fly-off competition against the Northrop/McDonnell-Douglas YF-23 for the Advanced Tactical Fighter contract. In April 1992 during flight testing after contract award, test pilot Tom Morgenfeld escaped without injury when the first YF-22 prototype that he was flying crashed while landing at Edwards Air Force Base in California. The cause of the crash was found to be a flight control software error that failed to prevent a pilot-induced oscillation.

The YF-22 was a developmental aircraft that led to the F-22; however, there are significant differences between the YF-22 and the F-22. Relocation of cockpit, structural changes, and many other smaller changes exist between the two types. The two are sometimes confused in pictures, often at angles where it is difficult to see certain features. For example, there are some F-22 with pitot booms which some think are only found on the YF-22.

The YF-22 was originally given the unofficial name "Lightning II", after the WWII fighter P-38, by Lockheed, which persisted until the mid-1990s when the USAF officially named the aircraft "Raptor". For a short while, the aircraft was also dubbed "SuperStar" and "Rapier". The F-35 later received the Lightning II name on July 7th 2006.

F-22 Raptor to F/A-22 and back again...

The production model was formally named F-22 "Raptor" when the first production-representative aircraft was unveiled on 9 April, 1997 at Lockheed-Georgia Co., Marietta, Georgia. First flight occurred on 7 September, 1997.
In September 2002, Air Force leaders changed the Raptor’s designation to F/A-22. The new designation, which mimicked that of the Navy’s F/A-18 Hornet, was intended to highlight plans to give the Raptor a ground-attack capability amid intense debate over the relevance of the expensive air-superiority jet. This was later changed back to simply F-22 on 12 December, 2005. On 15 December, 2005, the F-22A entered service.

Recent Developments...

In 2006, the Raptors development team, composed of Lockheed Martin and over 1,000 other companies, plus the United States Air Force, won the Collier Trophy, American aviations most prestigious award. The U.S Air Force will acquire F-22s that are to be divided among seven active duty combat squadrons, and jointly flown and maintained by three integrated Reserve and Air National Guard squadrons.

During Exercise Northern Edge in Alaska in June 2006, 12 F-22s of the 94th FS downed 108 adversaries with no losses in simulated combat exercises. In two weeks of exercises, the Raptor-led Blue Force amassed 241 kills against two losses in air-to-air combat, and neither Blue Force loss was an F-22.

This was followed with the Raptors first participation in a Red Flag exercise. 14 F-22s of the 94th FS supported attacking Blue Force strike packages as well as engaging in close air support sorties themselves in Red Flag 07-1 between February 3rd and February 16th 2007. Against designed superior numbers of Red Force Aggressor F-15s and F-16s, it established air dominance using eight aircraft during day missions and six at night, reportedly defeating the Aggressors quickly and efficiently, even though the exercise rules of engagement allowed for four to five Red Force regenerations of losses but none to Blue Force. Further, no sorties were missed because of maintenance or other failures, and only one Raptor was adjudged lost against the virtual annihilation of the defending force. When their ordnance was expended, the F-22s remained in the exercise area providing electronic surveillance to the Blue Forces.

While attempting its first overseas deployment to the Kadena Air Base in Okinawa, Japan, on 11 February, 2007, a group of six Raptors flying from Hickam AFB experienced multiple computer crashes coincident with their crossing of the 180th meridian of longitude (the International Date Line). The computer failures included at least navigation (completely lost) and communication. The fighters were able to return to Hawaii by following their tankers in good weather. The error was fixed within 48 hours and the F-22s continued their journey to Kadena.

On 30 April 2007, the National Museum of the Air Force announced that EMD Raptor 91-4003 would be put on display later in 2007 in the space being occupied by the YF-22. The Museum publicly unveiled its Raptor 91-4003 display on January 18th, 2008.

In 2007, tests carried out by Northrop Grumman, Lockheed Martin, and L-3 Communications enabled the AESA system of a Raptor to act like a WiFi access point, able to transmit data at 548 Megabit/sec and receive at Gigabit speed; far faster than the current Link 16 system used by US and allied aircraft, which transfers data at just over 1 Megabit/sec.

On November 22nd, 2007, F-22A Raptors of the 90th Fighter Squadron performed their first intercept of two Russian Tu-95MS Bear-H bombers in Alaska. This was the first time that F-22s had been called to support a NORAD mission.

On December 12th, 2007, Gen. John D.W. Corley, commander of Air Combat Command, officially declared the F-22s of the integrated active duty 1st Fighter Wing and Air National Guard 192nd FW fully operational, three years after the first Raptor arrived at Langley Air Force Base. This was followed from April 13th to April 19th, 2008 by an Operational Readiness Inspection (ORI) of the integrated wing in which it received an "excellent" rating in all categories while scoring a simulated kill-ratio of 221-0.

Specifications

Data from USAF, F-22 Raptor Team website, Lockheed Martin, Aviation Week, Journal of Electronic Defense (Sweetman 2000)

General Characteristics
  • Crew: 1
  • Length: 62 ft 1 in (18.90 m)
  • Wingspan: 44 ft 6 in (13.56 m)
  • Height: 16 ft 8 in (5.08 m)
  • Wing area: 840 ft² (78.04 m²)
  • Airfoil: NACA 64A?05.92 root, NACA 64A?04.29 tip
  • Empty weight: 31,670 lb (14,365 kg)
  • Loaded weight: 55,352 lb (25,107 kg)
  • Max takeoff weight: 80,000 lb (36,288 kg)
  • Powerplant: 2× Pratt & Whitney F119-PW-100 Pitch Thrust vectoring turbofans, 35,000+ lb (156+ kN) each
Performance
  • Maximum speed:
At altitude: Mach 2+ (1,325+ mph, 2,132+ km/h)
Supercruise: Mach 1.72 (1,140 mph, 1,825 km/h) at altitude
  • Range: 1,600 nmi (1,840 mi, 2,960 km) with 2 external fuel tanks
  • Combat radius: 410 nmi (471 mi, 759 km)
  • Ferry range: 2,000 mi (1,738 nmi, 3,219 km)
  • Service ceiling: 65,000 ft (19,812 m)
  • Wing loading: 66 lb/ft² (322 kg/m²)
  • Thrust/weight: 1.26
  • Maximum g-load: -3.5/+9.5 g
Armament
  • Guns: 1× 20 mm (0.787 in) M61A2 Vulcan gatling gun in starboard wing root, 480 rounds
  • Air to air loadout:
6× AIM-120 AMRAAM
2× AIM-9 Sidewinder
  • Air to ground loadout:
2× AIM-120 AMRAAM and
2× AIM-9 Sidewinder and one of the following:
2× 1,000 lb (450 kg) JDAM or
2× Wind Corrected Munitions Dispensers (WCMDs) or
8× 250 lb (110 kg) GBU-39 Small Diameter Bombs

Note: It is estimated that the internal bays can carry about 2,000 lb (910 kg) worth of bombs, and/or missiles. Four external hardpoints can be fitted to carry weapons or fuel tanks, each with a capacity of about 5 000 lb (2268 kg).

Avionics
  • RWR (Radar warning receiver): 250 nmi (463 km) or more
  • Radar: 125-150 miles (200-240 km) against 1 m² targets (estimated range).

Available link for download

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Sunday, February 26, 2017

Lockheed Boeing AC 130 Spectre Spooky Gunship

Lockheed Boeing AC 130 Spectre Spooky Gunship




The AC-130, solely used by the United States Air Force, is a turbo prop gunship variant of the C-130 Hercules. Although Lockheed was the designer of the original airframe, Boeing was responsible for the conversion of the Hercules to a gunship. There are two variants of the AC-130 which has two different names. The AC-130H Spectre and the AC-130U Spooky. The AC-130 has a standard crew of twelve-thirteen airmen, five of which are usually officers and the rest enlisted men.

The AC-130s are stationed at Hurlburt Airfield in Northwest Florida, part of the Air Force Special Operations Command (AFSOC), a component of the United States Special Operations Command (SOCOM).

Design...

AC-130s are heavily armed with many different weapons, even 105 mm howitzers. These weapons are fired from the side of the aircraft. They have both anti-personnel and anti-armor capabilities and are extremely accurate due to a continuous upgrade of on board systems such as radar.

The newer AC-130U Spooky variant is equipped with the AN/APQ-180, a synthetic aperture radar capable of detecting and identifying long-range targets. The airframe is much stronger with the integration of an armor protection system, or APS. It has an onboard GPS and an inertial navigation system. It also has twice the amount of munitions than the AC-130H. The AC-130U, employing technology developed in the 1990s, can attack two targets at one time with first round accuracy. Also, the Spooky has a higher service ceiling and longer range.

The older AC-130H Spectre variant, although it has half the amount of munitions capacity then the Spooky, is an excellent fire support platform. The Spectre is accurate enough to be able to place 105mm, 40mm, or 25mm munitions on targets with first round accuracy. The crews of these aircraft are extremely proficient working in military operations in urban terrain (MOUT) environments.

Operational History...
  • The AC-130 first appeared in Vietnam on September 27th, 1967 and began combat operations over Laos and South Vietnam.
  • By October 30th, 1968, enough AC-130 Gunship IIs arrived to form a squadron. The 16th Special Operations Squadron, or SOS, of the 8th Tactical Fighter Wing (TFW), at the Ubon Royal Thai Air Force Base in Thailand.
  • During the Vietnam War, the AC-130 was responsible for 10 000 trucks destroyed and participated in many crucial air support missions.
  • During the Invasion of Grenada (Operation Urgent Fury) in 1983, AC-130s were used to supress enemy defences enabling a successful assault of the Points Salines Airfield. One AC-130 crew won the Lieutenant General William H. Tunner Award for the mission.
  • AC-130s also participated in Operation Desert Storm. On January 31st, 1991, during the early morning hours, one AC-130H, AF Serial No. 69-6567, call sign Spirit 03, opted to stay and continue protecting the Marines despite the increasing threat of SAMs, or surface-to-air missiles. Unfortunately, Spirit 03 was shot down by a SAM and all fourteen crew members were KIA...
  • AC-130s participated in Operation Restore Hope and United Shield in Somalia.
  • AC-130s participated in the NATO mission in Bosnia-Herzegovina.
  • AC-130s participated in the 1997 evacuation of American noncombatants in Albania.
  • AC-130s were used in the buildup of US Forces in Iraq in 1998 the Iraqi government to comply with UN weapons inspections.
  • AC-130s participated in the 2001 invasion of Afghanistan and the Iraq War.
  • US Special Operations forces used AC-130s in 2007 on attacks on suspected al-Qaeda militants in Somalia.

The AC-130 has never lost a base under its protection to enemy forces.

World Records...

The AC-130 currently holds the record of the longest sustained flight. From the 22nd to the 24th of October 1997, two AC-130U Spookys flew 36.0 hours nonstop from Hurlbert Airfield, Florida to Taegu Air Base (Daegu), South Korea. There were altogether 7 air refuelings by KC-135 Stratotankers. This record shatted the previous one by over 10 hours and the two gunships took on 410 000 lb (184 500 kg) of fuel and displayed the Gunships ability to match their squadrons motto of Any Time, Any Place!.

Specifications...

General Characteristics (AC_130U)

Crew: 13
Officers: 5 (pilot, copilot, navigator, fire control officer, electronic warfare officer)
Enlisted: 8 (flight engineer, TV operator, infrared detection set operator, load master, four aerial gunners)
Length: 97 ft 9 in (29.8 m)
Wingspan: 132 ft 7 in (40.4 m)
Height: 38 ft 6 in (11.7 m)
Wing area: 1745.5 ft² (162.2 m²)
Loaded weight: 122,400 lb (55,520 kg)
Max takeoff weight: 155,000 lb (69,750 kg)
Powerplant: 4× Allison T56-A-15 turboprops, 4,910 shp (3,700 kW) each

Performance (AC-130U)

Maximum speed: 260 knots (300 mph, 480 km/h)
Range: 2,200 nm (2,530 mi, 4,070 km)
Service ceiling: 30,000 ft (9,100 m)

Armament

AC-130A Project Gunship II
4× 7.62 mm GAU-2/A miniguns
4× 20 mm M61 Vulcan cannon
AC-130A Surprise Package, Pave Pronto, AC-130E Pave Spectre
4× 7.62 mm GAU-2/A miniguns
2× 20 mm M61 Vulcan cannon
2× 40 mm (1.58 in) L/60 Bofors cannon
AC-130E Pave Aegis
2× 20 mm M61 Vulcan cannon
1× 40 mm L60 Bofors cannon
1× 105 mm (4.13 in) M102 howitzer

AC-130H Spectre
AC-130H Pave Spectre II
1× 40 mm L60 Bofors cannon
1× 105 mm (4.13 in) M102 howitzer
AC-130U "Spooky" Gunship
1× 25 mm (0.984 in) 5-Barrel GAU-12/U Equalizer Gatling gun
1× 40 mm L60 Bofors cannon
1× 105 mm (4.13 in) M102 howitzer


Available link for download

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Thursday, January 26, 2017

Lockheed Skunk Works SR 71 Blackbird

Lockheed Skunk Works SR 71 Blackbird


The SR-71B Blackbird, a trainer version of the SR-71. Note the dual cockpit to allow the instructor to fly the plane.

The SR-71 Blackbird is currently the 2nd fastest plane in the world, next to its predecessor, the A-12, which can reach speeds up to 3.35, while it is only capable of reaching Mach 3.2+. It was Designed by Clarence Kelly Johnson and produced by Lockheed Skunk Works, and flies at the edge of Space doing reconnaissance missions over Russia during the Cold War. Due to its high speed and amazing altitude, it could easily evade surface-air missiles (SAM). As a result, no Blackbird was lost to enemy action, though 12 of the 32 were lost in accidents. The Blackbird had been so effective that it was brought back out of retirement in the 1990s but was permanently retired in 1998.

The secret of the SR-71s high speed lies in its engines, and material used for its structure. Of course, they do not come cheap military wise. The Pratt & Whitney J58-P4 engine used on the Blackbird was the only military engine designed to operate continuously on afterburner. Also, incredibly, the J58 engine became more efficient when air speed increases, whereas conventional jet engines loses efficiency as the plane speeds up.

When the Blackbird reaches Mach 3, the friction between its surface and the air is so much that the heat generated could actually melt the surface of the aircraft. That is not the case when 85% of the surface of the Blackbird is made of titanium, while 15% of it is made of composite materials. This was a first in the airplane industry. The setback of using titanium is that is was extremely scarce, and very expensive. Additionally, much of the titanium sent to Lockheed to make the Blackbird was imported from the Soviet Union. Making it worse, 80% of the titanium initially delivered to Lockheed had to be rejected due to metallurgical contamination.

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