Thursday, July 29, 2010

Bomber Aircraft: SR-71 Blackbird


SR-71 BlackbirdFor 24 years, from 1966 through the 1980s, American leaders from field commanders to the President of the United States relied on data gathered by SR 71 Blackbird reconnaissance aircraft. Flying missions around the globe at speeds above Mach 3 and altitudes of 85,000 feet (26,000 m) or more, Blackbirds became a vital tool of international decision-making as their advanced photographic and electronic sensor systems collected intelligence for the Air Force and other federal agencies.



A congressional appropriation approved in late 1994 provided funds to return two or more SR-71s to reconnaissance flying. Subsequently, Lockheed Martin Skunk Works was awarded an Air Force contract to refurbish Blackbirds that had been kept in storage since 1990.

Program History



Origins of the SR 71 date back to the late 1950s when legendary Lockheed designer and Skunk Works founder Clarence L. "Kelly" Johnson proposed a high speed, high altitude alternative to supplement the Lockheed-built U-2 subsonic reconnaissance plane that would soon become vulnerable to Soviet missiles. As a result, the Blackbird family was initiated with the A 12, which first flew in April 1962. The single-seat A-12s were the smallest of the Blackbird series. Designed for reconnaissance missions, the A-12 spawned a two-place, armed version designated YF-12A, which was proposed as an interceptor. Although never adopted for this role, the YF-12s made important contributions as research aircraft, serving for more than a decade with NASA. It was the first aircraft capable of sustaining speeds above Mach 3.

A limited number of A 12 and YF 12 aircraft were produced before the design evolved into the SR-71, which first flew in 1964 and entered operational service in January 1966. Slightly larger than its predecessors, the SR-71 carried more fuel and featured chines that extended forward to the tip of the nose.

Blackbird Design
The aircraft remains a technological marvel. Practically every area of design required new approaches or breakthroughs in technology. To withstand high temperatures generated by friction in the upper atmosphere during sustained Mach 3 flight, the Blackbird required an array of specially developed materials including high temperature fuel, sealants, lubricants, wiring and other components. Ninety-three percent of the Blackbird's airframe consists of titanium alloy that allows the aircraft to operate in a regime where temperatures range from 450 degrees Fahrenheit at its aft midsection to 950 degrees Fahrenheit near the engine exhaust. The cockpit canopy, made of special heat resistant glass, must withstand surface temperatures as high as 640 degrees Fahrenheit.

Two Pratt & Whitney J58 turbojet engines with afterburners, each supplying more than 35,000 pounds of thrust, are housed in wing nacelles with diameters larger than the fuselage itself. Virtually every part of these complex powerplants had to be fabricated from special materials to meet the demands of triple-sonic flight. A translating (moveable) spike in each inlet controls airflow, retracting at speeds above Mach 1.6 to capture more air for the engines.

Accomplishments
Although its many contributions to national security will never be fully revealed to the public, the SR-71 holds many world aviation records for speed and altitude.

In 1971 an Air Force crew demonstrated the SR-71's extended supersonic capabilities on a non-stop, 15,000-mile (24,140 km) flight -- the equivalent of a non-stop trip from San Francisco to Paris and back -- in 10-1/2 hours. Slowing to subsonic speeds for periodic aerial refueling, the Blackbird still averaged nearly 1,500 mph. For this feat the crew was awarded the 1971 Mackay trophy for "most meritorious flight of the year" and the 1972 Harmon International Trophy for the "most outstanding international achievement in the art/science of aeronautics."

On Sept. 1, 1974, an SR-71 flew from New York to London in 1 hour, 54 minutes, 56 seconds, smashing the previous trans-Atlantic speed record by nearly three hours! Returning to the U.S. on Sept. 13, 1974, the same aircraft established a world speed record of 3 hours, 47 minutes, 36 seconds for the 5,463 mile (8,790 km) flight from London to Los Angeles. It literally outraced the sun, landing some four hours before the time of day it took off.

Three SR-71s flown by three different crews set seven world speed and altitude records on July 27 and 28, 1976. They captured three records previously held by a specially modified Russian MiG 25 Foxbat and bettered four records held by the Lockheed/USAF YF-12. The new marks included absolute and class records of 2,193 mph (3,530 kph) for speed over a straight course and 85,069 feet (25,930 m) for altitude in sustained level flight.



Specifications: (SR-71)
Span: 55’ 7”
Length: 107’ 5”
Height: 18’ 6”
Weight: 170,000 lb.
Max Speed: 2,000 + mph
Rate of Climb: 1,140 ft/min
Service Ceiling: 85, 000 + ft
Range: 2,900 + miles


In achieving these milestones the SR-71 was never extended to its ultimate capabilities. The aircraft used were stock, operational SR-71s, unlike the specially prepared aircraft commonly used to set such records. Air Force crews always stayed well within the SR-71's normal operational envelope.

In January 1990 the Air Force officially retired its fleet of SR-71s from service. On March 6, 1990, aircraft number 17972, the same aircraft that had set the 1974 records, was delivered to the Smithsonian Institution for permanent display at Dulles International Airport. Enroute, flying at "normal" operating speeds, this SR-71 set four more world records including a Los Angeles to Washington, D.C., flight time of 64 minutes, 2 seconds, averaging 2,144 mph (3,452 kph). That was the last SR-71 mission flown by an Air Force crew until the spring of 1995, when the crew retraining program began.

Between 1990 and 1995, NASA crews at the Dryden Flight Research Facility at Edwards AFB flew two SR-71s for training and scientific flights, and kept a third in storage. Those Blackbirds had been loaned to NASA by the Air Force when the military flying ceased.

The Skunk Works received funding to refurbish two Blackbirds to operational capability -- they were delivered to the U.S. Air Force in 1995.

For more SR-71 Blackbird photos visit the SR-71 set of Flickr collection
Click Here


Tuesday, July 27, 2010

Bomber Aircraft: Boeing B-52 Stratofortress Intercontinental Strategic Bomber



The B-52 Stratofortress is a long-range, strategic heavy bomber capable of dropping or launching the widest array of weapons in the U.S. inventory. The latest version, the B-52H, can carry up to 20 air-launched cruise missiles.



Used for strategic attack, air interdiction, offensive counter-air and maritime operations, its capabilities include:
  • Carrying nuclear or precision-guided conventional ordnance, including gravity bombs, cluster bombs, precision guided missiles and joint direct attack munitions
  • Delivering approximately 70,000 pounds of mixed payload, both internally and on external pylons
  • Combat range exceeding 8,800 miles (7,652 nautical miles) unrefueled -- can be refueled aerially
  • High subsonic speeds up to 650 miles per hour, or Mach 0.86
  • Flying at altitudes up to 50,000 feet (15,166.6 meters)
  • Low-altitude flight capability, augmented by its electro-optical viewing system


The B-52 entered military service in 1954. Ongoing updates have included new avionics, data-link communications, electronic defense and offensive systems, and more powerful, fuel-efficient turbofan engines. Used in Operation Iraqi Freedom, the B-52 has been the longest-serving bomber U.S. military history.

HISTORY:
First Flight 15 April 1952 Service Entry February 1955
Retirement B-52D 1983, B-52G 1994, B-52H not planned until at least 2020

CREW:
Five: aircraft commander, pilot, radar navigator, navigator, electronic warfare officer

ESTIMATED COST:
$53.4 million [1998$]

AIRFOIL SECTIONS:
Wing Root NACA 63A219.3 mod Wing Tip NACA 65A209.5 mod

DIMENSIONS:
Length 160.92 ft (49.05 m) Wingspan 185.00 ft (56.39 m) Height 40.67 ft (12.40 m) Wing Area 4,000 ft2 (371.6 m2)
Canard Area not applicable



WEIGHTS:
Empty 195,000 lb (88,450 kg) Normal Takeoff unknown
Max Takeoff B-52A-F = 452,000 lb (205,025 kg),
B-52G/H = 488,000 lb (219,600 kg) Fuel Capacity internal: unknown
external: unknown Max Payload 70,000 lb (31,500 kg)

    PROPULSION:

Powerplant eight Pratt & Whitney TF33-P-3/103 turbofans
Thrust 136,000 lb (605.0 kN)

PERFORMANCE:
Max Level Speed at altitude: 595 mph (955 km/h) [B-52H] at sea level: 405 mph (650 km/h), Mach 0.53 cruise speed: 510 mph (820 km/h) Initial Climb Rate unknown Service Ceiling 50,000 ft (15,240 m) Range typical: 6,380 nm (11,800 km) ferry: 8,685 nm (16,090 km) g-Limits unknown

ARMAMENT:
Gun one 20-mm Vulcan cannon in tail (remotely controlled, but removed by 1991 to save money) Stations one internal bomb bay and four external hardpoints
Air-to-Surface Missile up to 20 AGM-69 SRAM or AGM-86 ALCM, up to 8 AGM-84 Harpoon, up to 4 AGM-142 Popeye
(B-52H) up to 20 AGM-86C CALCM, up to 20 AGM-129 ACM, AGM-154 JSOW, AGM-158 JASSM
Bomb up to 8 B61/B83 nuclear bombs, up to 51 Mk 82 500-lb GP, Mk 84 2000-lb GP, up to 51 M117 750-lb GP, GBU-30 JDAM, CBU-87/89/97 cluster, CBU-103/104/105 WCMD
(B-52D) up to 108 conventional bombs Other maritime mines

KNOWN VARIANTS:
XB-52 and YB-52 Prototypes B-52A Boeing test and development aircraft; 3 built B-52B First operational model for the USAF; 50 built
RB-52B Reconnaissance version based on the B-52B model; 27 converted B-52C Improved model with better equipment and greater performance; 35 built
B-52D New fire-control system for four 0.5-in. machine gun assembly in tail; 170 built, retired from service in 1983 B-52E Improved navigation and weapons systems, new flight deck layout to accomodate improved displays, improved engine; 100 built B-52G Lighter airframe and greater fuel capacity; originally designed to operate AGM-28 Hound Dog missile and also equipped with 'Quail' decoy aircraft; 193 built B-52H Improved engine, better low-level performance, new tail gun; 102 built EB-52 Proposal to fit B-52 airframes with electronic warfare equipment for use as stand-off jammers

KNOWN COMBAT RECORD:
Vietnam War (USAF, 1965-1972)
Iraq - Operation Desert Storm (USAF, 1991)
Iraq - Operation Southern Watch (USAF, 1991-2003)
Iraq - Operation Desert Strike (USAF, 1996)
Iraq - Operation Desert Fox (USAF, 1998)
Kosovo - Operation Allied Force (USAF, 1999)
Afghanistan - Operation Enduring Freedom (USAF, 2001)
Iraq - Operation Iraqi Freedom (USAF, 2003)

KNOWN OPERATORS: United States (US Air Force),
United States (US Air Force Reserves)

Monday, July 26, 2010

Bomber Aircraft: Rockwell B-1B Lancer Intercontinental Strategic Bomber






Based on the B-1A bomber, the B-1B was developed by Rockwell International in the 1980s, when 100 of the aircraft were produced to support a nuclear mission and were stationed at Strategic Air Command (SAC) bases. In the 1990s, the B-1B was transitioned to a conventional-weapons mission.

Nuclear Mission Capabilities

From 1985 to 1997, the B-1B supported a nuclear mission with the following capabilities:

* High-speed flight of Mach 1.25
* Gross takeoff weight of 477,000 pounds
* The AGM-69A nuclear short-range attack missile (SRAM)
* Westinghouse synthetic aperture radar and offensive-defensive avionics systems

Conventional Mission Capabilities

With the end of the cold war, the B-1Bs were converted to support conventional munitions, and 32 of them were retired beginning in 2001 The 68 remaining B-1Bs retain the speed, payload and targeting capabilities along with the following new conventional enhancements, which were introduced in phases by Boeing:
  • Hardware and software enhancements to accommodate a broad range of conventional gravity weapons such as 24 Mk84 bombs, 84 Mk82 bombs or 30 conventional bomb units.
  • Global positioning system (GPS) navigation, joint direct attack munitions (JDAM), anti-jam radios, and the ALE-50 towed decoy countermeasure

  • New mission computers, wind compensated munitions dispensers (WCMDs), the joint stand-off weapon (JSOW), the joint air-to-surface stand-off missile (JASSM), and the ability to employ multiple types of weapons simultaneously from the three weapons bays.


Future capabilities include new digital radios, cockpit display and sensor improvements improved electronic countermeasures systems, radar warning receivers, external carriage capability and new weapons.
Combat Service and Awards

The B-1B has been distinguished by the following combat activity and awards:
  • Combat operations including Desert Fox (Iraq, 1998), Allied Force (Kosovo, 1999), Enduring Freedom (Afghanistan, 2001+), Iraqi Freedom (2003+)
  • A very high ratio of precision guided munitions dropped per combat sortie -- from a maximum ratio of 1% of sorties delivering 22% of the guided weapons in Iraqi Freedom (1:22) to a minimum ratio of 5% of sorties delivering 70% of the JDAM weapons in Afghanistan (5:70)
  • 100 world records for speed, payload, and distance


HISTORY:
First Flight (B-1A) 23 December 1974
(B-1B) 18 October 1984
Service Entry 1 October 1986

CREW:
four: pilot, copilot, 2 electronic warfare/weapon systems officers

ESTIMATED COST:
$283 million [1998$]

AIRFOIL SECTIONS:
Wing Root unknown
Wing Tip unknown

DIMENSIONS:Length: 147.00 ft (44.81 m)Wingspan unswept: 136.71 ft (41.67 m)swept: 78.21 ft (23.84 m)Height: 34.83 ft (10.36 m)Wing Area 1,950 ft² (181.2 m²)Canard Area: unknown



WEIGHTS:
Empty:192,000 lb (87,090 kg)Normal Takeoff unknown Max Takeoff: 477,000 lb (216,365 kg)Fuel Capacity internal: unknown external: unknown Max Payload 80,000 lb (36,290 kg)

PROPULSION: Powerplant four General Electric F101-102 afterburning turbofans Thrust 123,120 lb (547.7 kN) with afterburner

PERFORMANCE:
Max Level Speed at altitude: 1,000 mph (1,600 km/h) at 36,090 ft (11,000 m), Mach 1.5 at sea level: 750 mph (1,205 km/h), Mach 0.99
low-level mission: 600 mph (965 km/h) at 200 ft (61 m)
Initial Climb Rate unknown
Service Ceiling unknown
Range 6,090 nm (11,265 km)
g-Limits unknown

ARMAMENT:
Gun none Stations three internal weapons bays and fourteen external hardpoints Air-to-Surface Missile originally up to 38 AGM-69 SRAM or 22 AGM-86 ALCM [no longer permitted under START] up to 12 AGM-154 JSOW, up to 24 AGM-158 JASSM Bomb originally up to 26 B28/B43 or 24 B61/B83 nuclear bombs [no longer permitted under START], up to 84 Mk 82 GP, up to 24 Mk 84 GP, up to 24 GBU-31 JDAM, up to 30 CBU-87/89/97 cluster, up to 30 CBU-103/104/105 WCMD Other up to 84 Mk 36 or Mk 62 500-lb sea mines, up to 8 Mk 85 sea mines

KNOWN VARIANTS:
B-1A Original design with less-refined aerodynamics but capable of Mach 2 at altitude, was cancelled in 1977 in favor of rearming the B-52 with cruise missiles; 4 prototypes built
B-1B Production model with an improved shape for greater stealth and better flight performance at low altitudes; 100 built
EB-1B Proposal to modify B-1B airframes as stand-off electronic warfare jamming platforms to replace the EA-6B Prowler jamming aircraft
B-1R Boeing proposal to rebuild the existing B-1B fleet as a "regional" fighter bomber force by replacing the F101 engines with the F119 turbofan used in the F-22 to increase speed to Mach 2.2 but at the cost of reduced range, the rebuilt bomber would carry an AESA radar for improved targeting and would serve as a "truck" carrying a large payload of bombs, air-to-ground missiles, and air-to-air missiles

KNOWN COMBAT RECORD:
  • Iraq - Operation Southern Watch (USAF, 1998-2003)

  • Iraq - Operation Desert Fox (USAF, 1998)

  • Kosovo - Operation Allied Force (USAF, 1999)

  • Afghanistan - Operation Enduring Freedom (USAF, 2001-present)

  • Iraq - Operation Iraqi Freedom (USAF, 2003-present)


KNOWN OPERATORS:
  • United States (US Air Force)

  • United States (US Air National Guard)


US AIRCRAFT CARRIER






Aircraft carriers provide a wide range of possible response for the National Command Authority.

The aircraft carrier continues to be the centerpiece of the forces necessary for forward presence. Whenever there has been a crisis, the first question has been: "Where are the carriers?" Carriers support and operate aircraft that engage in attacks on airborne, afloat, and ashore targets that threaten free use of the sea; and engage in sustained operations in support of other forces.

Aircraft carriers are deployed worldwide in support of U.S. interests and commitments. They can respond to global crises in ways ranging from peacetime presence to full-scale war. Together with their on-board air wings, the carriers have vital roles across the full spectrum of conflict.

The Nimitz-class carriers, nine operational and one under construction, are the largest warships in the world. USS Nimitz (CVN 68) was the first to undergo its initial refueling during a 33-month Refueling Complex Overhaul at Newport News Shipbuilding in Newport News, Va., in 1998. The next generation of carrier, the GERALD R. FORD Class (the lead ship hull number will be CVN 78), is programmed to start construction in 2007 and is slated to be delivered in 2015 to replace USS Enterprise (CVN 65). CVN 79 is programmed to begin construction in 2012 and to be placed in commission in 2018.

The Carrier Mission is:
  • To provide a credible, sustainable, independent forward presence and conventional deterrence in peacetime,
  • To operate as the cornerstone of joint/allied maritime expeditionary forces in times of crisis, and
  • To operate and support aircraft attacks on enemies, protect friendly forces and engage in sustained independent operations in war.


THREE OF THE US AIRCRAFT CARRIER
General Characteristics, Nimitz Class
Builder: Newport News Shipbuilding Co., Newport News, VA.
Date Deployed:
May 3, 1975 (USS Nimitz).
Unit Cost:
About $4.5 billion each.
Propulsion: Two nuclear reactors, four shafts.
Length:
1,092 feet (332.85 meters).
Beam:
134 feet (40.84 meters); Flight Deck Width: 252 feet (76.8 meters).
Displacement:
Approximately 97,000 tons (87,996.9 metric tons) full load.Speed: 30+ knots (34.5+ miles per hour).
Crew:
Ship's Company: 3,200 - Air Wing: 2,480.
Armament:
Two or three (depending on modification) NATO Sea Sparrow launchers, 20mm Phalanx CIWS mounts: (3 on Nimitz and Dwight D. Eisenhower and 4 on Vinson and later ships of the class.).
Aircraft:
85.
Ships:
USS Nimitz (CVN 68), San Diego, CAUSS Dwight D. Eisenhower (CVN 69), Norfolk, VAUSS Carl Vinson (CVN 70), Newport News, VAUSS Theodore Roosevelt (CVN 71), Norfolk, VAUSS Abraham Lincoln (CVN 72), Everett, WAUSS George Washington (CVN 73), Norfolk, VAUSS John C. Stennis (CVN 74), Bremerton, WAUSS Harry S. Truman (CVN 75), Norfolk, VAUSS Ronald Reagan (CVN 76), San Diego, CAGeorge H.W. Bush (CVN 77) - (Christened 7 October 2006)




General Characteristics, Enterprise Class

Builder: Newport News Shipbuilding Co., Newport News, VA. Date Deployed: November 25, 1961 (USS Enterprise). Propulsion: Eight nuclear reactors, four shafts.Length: 1,101 feet 2 inches (335.64 meters).Beam: 133 feet (39.9 meters); 252 feet (75.6 meters).Displacement: 89,600 tons ( 81,283.8 metric tons) full load. Speed: 30+ knots (34.5 miles per hour).Crew: Ship's Company: 3,350 - Air Wing 2,480. Armament: Two Sea Sparrow missile launchers, three Phalanx 20 mm CIWS mounts. Aircraft: 85. Ships:USS Enterprise (CVN 65), Norfolk, VA


General Characteristics, Kitty Hawk Class

Builder: New York Ship Building Corp., Camden, NJ.Date Deployed: April 29, 1961 (USS Kitty Hawk).Propulsion: Eight boilers, four geared steam turbines, four shafts, 280,000 shaft horsepower.Length: 1062.5 feet (323.8 meters).Beam: 130 feet (39 meters); Flight Deck Width: 252 feet (76.8 meters).Displacement: Approx. 80,800 tons (73,300.5 metric tons) full load.Speed: 30+ knots (34.5+ miles per hour).Crew: Ship's Company: 3,150 - Air Wing: 2,480.Armament: Sea Sparrow launchers, 3 20mm Phalanx CIWS mounts.Aircraft: 85.Ships:USS Kitty Hawk (CV 63), Yokosuka, Japan

War Aircraft: F-22



Welcome to the era of the F-22 Raptor – the world’s premier 5TH generation fighter.

The F-22 is the only fighter capable of simultaneously conducting air-to-air and air-to-ground combat missions with near impunity. This is accomplished with a never-before-seen standard of survivability even while facing large numbers of sophisticated airborne and ground-based threats.

In addition to being America’s most prominent air-superiority fighter, the F-22 evolved from its original concept to become a lethal, survivable and flexible multimission fighter. By taking advantage of emerging technologies the F-22 has emerged as a superior platform for many diverse missions including intelligence gathering, surveillance, reconnaissance and electronic attack.

The Raptor is operational today, protecting our homeland and combat ready for worldwide deployment. Two squadrons of F-22s are assigned to Air Combat Command’s 1st Fighter Wing at Langley AFB, Va. And two squadrons are assigned to the 3rd Wing at Elmendorf AFB, Alaska. Raptor pilots and maintainers train at Tyndall AFB, Fla., while operational testing is conducted at Edwards AFB, Calif., and Nellis AFB, Nev. New F-22s continue to roll from the production line and will soon operate out of Holloman AFB, N.M., and Hickam AFB, Hawaii.