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The de Havilland Comet


The de Havilland Comet, the world's first ever commercial jet airliner to reach production. Developed and manufactured by de Havilland, the Comet was considered a landmark British aeronautical design. It not only revolutionised air travel but also brought the world closer together with its high speed, compared to older turbo prop planes.

Although not used in the commercial world, the Comet's military derivative, Hawker Siddeley Nimrod, is still in service and is expected to serve the Royal Air Force until the 2020s, almsot 70 years after its first flight.

Design and Development...

The Comet was designed to fulfill the need for a transatlantic airliner and Sir Geoffrey de Havilland, head of the de Havilland company, used his power and influence, plus his company's expertise with jets, to persuade the Brabazon Commitee that a transatlantic jet mailplane is needed after the war. Subsequently, the Commitee accepted de Havilland's proposal, calling it the Type IV (of five designs), and awarded the production contract to de Havilland's DH.106. The British Overseas Airways Corporation (BOAC) found the Type IV rather attractive and in the last month of 1945, agreed to buy ten aircraft.

The Type IV was officially christened Comet in December 1947. First deliveries were expected five years later. The first flight of the Comet was held on July 27th, 1949, and lasted for 31 minutes, by de Havilland Chief Test Pilot John Cunningham, a famous wartime night-fighter pilot. It was then publicly displayed at the 1949 Farnborough Airshow before beginning flight trials. A second prototype made its maiden flight a year later.

The Comet has an all-metal low-wing cantilever monoplane, and was powered by four jet engines. About the size of a Boeing 737, the Comet was quite luxurious for the first jet airliner. There was lots of room, with 36 seats to each aircraft, and each had its own ashtray. The galley served hot and cold food and drinks, and there was even a bar. Men's and Women's washrooms were seperate, which is something you don't see on modern airliners, and the passenger cabin was much quieter compared to its propeller-driven airliners counter-parts. The Comet's four-man cockpit held two pilots, a navigator and flight engineer. The Comet was also the first pressurised jet-propelled commercial aircraft.

de Havilland's clean, low-drag design featured many unique or innovative design elements, including a swept leading edge, integral wing fuel tanks and four wheel bogie main undercarriage units. Emergencies were countered with lift rafts, which were storeed in the wings near the engines and every seat had a life vest stowed under each seat bottom.

The Comet was powered by two de Havilland Ghost 50 Mk1 turbojet engines buried in the wings close to the fuselage. British engineers chose this configuration as it avoided the drag created by podded engines and allowed fin and rudder, since the hazards of asymmetric, or non-balanced thrust, were reduced. The engines' higher mounting on the wings also lessened the risk of ingestion damage, which is a major problem for turbine engines. However, this design does have its setbacks, such as increased structural weight and complexity of the air frame, as well as a higher chance for wing failure when an engine is on fire, which was cited as the main reason Boeing Aircraft Company chose podded engines over engines buried in the wings.

The Comet's skin is a composition of new and advanced alloys, chemically bonded together with Redux, which is a type of epoxy adhesive, and riveted. It saved weight and reduced the risk of fatigue cracks spreading from the rivets.

Testing...

When the Comet went into service on May 2nd, 1952, it was the most exhaustively tested airliner in history. Water tanks were used to test airframe for metal fatigue by repeatedly pressuring and depressuring the airframe through more than 16 000 cycles, which is equivalent to about 40 000 hours of airline service. The windows were also tested to their max capabilities, and one window frame survived a massive 100 psi, which about 1 250% over the maximum pressure it would encounter in service.

Early Comet disasters...

Early versions of the Comet suffered from catastrophic metal fatigue, which was the root cause of a string of well-publicised accidents. The first of these occured on January 10th, 1954 when Comet G-ALYP ("Yoke Peter"), BOAC Flight 781, broke up in flight mysteriously and crashed into the Mediterranean off the coast of the Italian island Elba. There were no survivors. The entirely Comet fleet was subsequently grounded while the Abell Commitee met to determine the cause of the crash. The conclusion was fire, and modifications were made to the aircraft to protect the engines and wings from damage which might start another fire. However, three months later, another crash of the sort occured in the waters near Naples. Investigators were extremely puzzled and a large investigation board was formed under the direction of the Royal Aircraft Establishment (RAE). They subjected Comet airframes to pressurisation cycles and found the cause of the crashes was metal fatigue. The Comets were redesigned and most served with the military, until 1958 when it resumed commercial service, by which time the much-improved Comet 4 was introduced, and became the first jet airliner to enter transatlantic service. However, by then, United States aircraft manufacturers caught up with Boeing's 707 jetliner and Douglas' DC-8, which were both faster and cost effective, rendering the Comet less profitable. De Havilland later went on to long-range missiles, and in 1962 went back to the airline world with the three-engine jetliner, Trident, but was beat again by Boeing with its 727, also a tri-jet.

De Havilland's hard-learned lessons benefited aircraft manufacturers all over the world, and according to John Cunningham, representatives from Boeing and Douglas "admitted that if it had not been for our problems, it would have happened to them." [Faith 1996, pp. 158-165]

Specifications... (Comet 4)

General characteristics

Crew: 4
Capacity: 56-109 passengers
Length: 34 m (112 ft)
Wingspan: 35 m (115 ft)
Height: 9 m (30 ft)
Wing area: 2,120 ft² (197 m²)
Airfoil: NACA 63A116 mod root, NACA 63A112 mod tip
Empty weight: 75,400 lb (34,200 kg)
Loaded weight: 162,000 lb (73,470 kg)
Powerplant: 4× Rolls-Royce Avon Mk 524 turbojets, 10,500 lbf (46.8 kN) each

Performance

Maximum speed: 500 mph (430 kn, 810 km/h)
Range: 2,800 nmi (3,225 mi, 5,190 km)
Service ceiling: 40,000 ft (12,000 m)

Northrop Grumman B-2 Spirit

The B-2 Spirit, commonly known as the Stealth Bomber, is a multirole heavy bomber with "low observable" stealth technology capable of penetrating into dense anti-aircraft defences and drop conventional or nuclear bombs. It is highly stealthed and very hard to detect. However, this is a very expensive bomber, costing the US almost 2 billion to build one, and even more to maintain it.

Although designed for Cold War scenarios, the B-2 has been used to drop bombs in Kosovo in the late 1990's and in the ongoing wars in Iraq and Afghanistan.
Due to the bombers 'out-of-this world' looks and technology, it has been a prominent public spectacle at air shows since the 1990's and has been the subject of espionage and counter-espionage activities.

Development...

The Northrop YB-49 and Horten Ho 229 flying wing designs of the 1940s preceded the B-2. The Spirit originated from the Advanced Technology Bomber (ATB) black project that began in 1979. Meanwhile, as Ronald Reagan campaigned for the Presidency in 1979 and 1980, he promised a restoration of American military strength. On August 22, 1980, the Department of Defense first publicly disclosed that it was working to develop stealth aircraft including the ATB. The ATB competition was reduced to the Northrop/Boeing and Lockheed/Rockwell teams with each receiving a study contract for further work. Both teams developed flying wing designs. The Northrop design was larger while the Lockheed design was smaller and included a small tail.

The Northrop/Boeing team's ATB design was selected over the Lockheed/Rockwell design on October 20, 1981. The black project was funded under the code name "Aurora". The Northrop design would receive the designation B-2 and the name "Spirit". The bomber's design was changed in the mid-1980s when its mission profile was changed from high-altitude to low-altitude, terrain-following. The redesign delayed the B-2's first flight by two years and added about US$1 billion to the program's cost. An estimated US$23 billion was secretly spent for research and development on the B-2 by 1989. At the program's peak, 13,000 people were employed at a dedicated plant in Pico Rivera, California for the plane's engineering and portions of its manufacturing.

The B-2 was first publicly displayed on November 22, 1988, at Air Force Plant 42, Palmdale, California, where it was built. Its first public flight was on July 17, 1989 from Palmdale. The B-2 Combined Test Force, Air Force Flight Test Center, Edwards Air Force Base, is responsible for flight testing Air Force aircraft.

A procurement of 132 aircraft was planned in the mid-1980s, but this was later reduced to 75. Yielding to budgetary pressures and congressional opposition, in his 1992 State of the Union Address, President George H.W. Bush announced total B-2 production would be limited to 20 aircraft. This reduction was largely a result of the disintegration of the Soviet Union, which effectively rendered void the Spirit's primary Cold War mission.



Design...

The B-2 Spirit, as you know it, is designed for stealth and not payload. It is nuclear capable, however, and it can penetrate most of the sophisticated anti-aircraft radars without being detected. The B-2's stealth characteristics are due to its air frame and the special paint coating for maxed stealth. Also, it not only has very reduced radar signature but also reduced acoustic, infrared, and visual detectability as well.

B-2's ability steath capabilities originated from the F-117 Nighthawk, which was one of the first stealth-capable operational aircraft. Both aircraft were made possible due to a Russian-born physicist and mathematician, Pyotr Ufimtsev's, theoritical work.

The B-2 has a crew of two due to the replacement of the duties of many people by the computer. The mission commander seats on the right and the pilot on the left. The B-2's unconventional flying wing design results to control difficulties so much so that it is mostly flown by a highly advanced on board computer. The B-2 is also highly automated so a crew member can use the toilet, prepare hot food, or sleep while the other monitors the aircraft.

Congress recently funded upgrades to the B-2's weapons systems in 2008.

Operational History...

  • Kosovo War
  • War in Afghanistan
  • War in Iraq

During the Iraq War, B-2s dropped a total of 1.5 million pounds of munitions.

Costs...

The B-2 is the mostly costly plane to be built in the world. The program itself costed US 44.75 billion in total in 1997 dollars (projected through 2004) which includes development, procurement, facilities, construction, and spare parts, and each unit cost about US $737 million (1997 air vehicle cost per plane). That's just the initial costs. Maintainence for the B-2 is horrific due to the cost for its air-conditioned hangars large enough for the bomber's 172 ft wingspan, which is required for the B-2 to maintain the aircraft's stealth properties and especially its "low-observable" stealthy skins. In addition, each hour of flight for the B-2 results to a whopping 119 hours of maintenance on the ground, a lot considering the B-52 only needs 53 hours and the B-1, 60 hours.

The total program cost for one B-2 averaged US$2.13 billion. There are currently 20 B-2 aircraft in active service; only a total of 21 were built.

A Costly Accident...

On February 23rd, 2008, a B-2 crashed on the runway shortly after the takeoff in the Andersen Air Force Base in Guam. The two crew man ejected and survived, but the aircraft, Spirit of Kansas, 89-0127, was completely destroyed, resulting a hull loss estimated at US$1.4 billion. It had been operated by the 393rd Bomb Squadron, 509th Bomb Wing, Whiteman Air Force Base, Missouri, and it had logged 5 176 flight hours.

Specifications...

(Data from USAF Fact Sheet, Pace, Spick, Globalsecurity)

General characteristics

Crew: 2
Length: 69 ft (21.0 m)
Wingspan: 172 ft (52.4 m)
Height: 17 ft (5.18 m)
Wing area: 5,140 ft² (478 m²)
Empty weight: 158,000 lb (71,700 kg)
Loaded weight: 336,500 lb (152,200 kg)
Max takeoff weight: 376,000 lb (170,600 kg)
Powerplant: 4× General Electric F118-GE-100 non-afterburning turbofans, 17,300 lbf (77 kN) each

Performance

Maximum speed: Mach 0.95 (525 knots, 604 mph, 972 km/h)
Cruise speed: Mach 0.85 (470 knots, 541 mph, 870 km/h)
Range: 6,000 nmi (11,100 km, 6,900 mi)
Service ceiling: 50,000 ft (15,200 m)
Wing loading: 67.3 lb/ft² (329 kg/m²)
Thrust/weight: 0.205

Armament

2 internal bays for 50,000 lb (22,700 kg) of ordnance.
80× 500 lb class bombs (Mk-82) mounted on Bomb Rack Assembly (BRA)
36× 750 lb CBU class bombs on BRA
16× 2000 lb class weapons (Mk-84, JDAM-84, JDAM-102) mounted on Rotary Launcher Assembly (RLA)
16× B61 or B83 nuclear weapons on RLA

Later avionics and equipment improvements allow B-2A to carry JSOW and GBU-28s as well. The Spirit is also designated as a delivery aircraft for the AGM-158 JASSM when the missile enters service.

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-130's 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-130's 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 1990's, 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 Gunship's ability to match their squadron's 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

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