旅遊指南

The Most Numerous US Navy Aircraft By Type

The US Navy has numerous aircraft in its fleet. Each aircraft serves a vital purpose in furthering the Navy’s global mission. The most well-known and perhaps visible are fighter aircraft, which routinely appear in news stories and video clips.

While these aircraft are undoubtedly vital, the Navy also employs refueling, cargo, surveillance and reconnaissance, antisubmarine combat, various helicopters, and the humble training aircraft.

In this article, we dive into the Navy’s most numerous aircraft by type. Additionally, we will take a brief look at their individual histories and the role they play in the service of the US Navy.

The SH-60 Seahawk

Inventory: 454 with 3 on order

The Seahawk is a workhorse helicopter specializing in anti-surface and anti-submarine warfare. However, the Seahawk also performs search and rescue, medical evacuation, special warfare, and vertical replenishment operations.

Photo: US Navy

During the 1970s, the US Navy began searching for a replacement for the Kaman SH-2 Seasprite, which entered the Navy’s inventory in 1962. For a replacement, the Navy based its new maritime requirements on the Army’s

Related

UH-60 Black Hawk

The Black Hawk fulfills a wide range of missions in the US Army – and even more outside of Army service.

in order to achieve commonality and avoid a lengthy design and testing process. In so doing, the Seahawk maintains an 83% commonality with the Blackhawk.

Technical notes for the SH-60 Seahawk

General Specifications

Related Data

Contractor(s)

Sikorsky Aircraft Corporation (airframe); General Electric Company (engines); IBM Corporation (avionics components).

Propulsion

Two General Electric T700-GE-700 or T700-GE-701C engines; thrust: up to 1,940 shaft horsepower.

Length

64 feet 10 inches (19.6 meters).

Height

Varies with the version; from 13 to 17 feet (3.9 to 5.1 meters).

Rotor Diameter

53 feet 8 inches (16.4 meters).

Weight

Varies; 21,000 to 23,000 pounds (9,450 to 10,350 kg).

Airspeed

180 knots maximum.

Range

Generally about 380 nautical miles (600 km); range becomes unlimited with air refueling capability.

Crew

Three to four

The F/A-18 Super Hornet entered the fleet in 1999, replacing the F-14 Tomcat.

Some of the primary changes made to fit the Seahawk into naval operations include enhanced corrosion protection, more powerful T700 engines, removal of the left-side door, additional weapons pylons, and a 25-tube sonobuoy launcher. Additional structural changes were made for ease of operations from naval vessels.

schematic of a Seahawk

Photo: Sikorski

Related

The Aircraft Replacing the US Navy’s MH-60 Seahawk Helicopter Fleet

The Navy is just beginning to consider a replacement for the Seahawk, with its ideas influenced by the Army’s tiltrotor design.

The Seahawk is equipped with a sophisticated set of sensors to carry out its anti-surface and anti-submarine warfare roles. These include a towed Magnetic Anomaly Detector, APS-124 search radar, ALQ-142 ESM system, and an optional nose-mounted Forward-Looking Infrared turret.

In terms of weapons, the Seahawk can carry the Mk 46, Mk 50 or the Mk 54 torpedo. Additionally, this aircraft can carry the Penguin and AGM-114 Hellfire missiles. As far as self-defense armament, the Seahawk can mount an M60/M240, 7.62 machine gun or the GAU-16 .50-caliber machine gun.

The F/A-18 Super Hornet

Inventory: 421 with 76 on order

Following the Vietnam War, the US Navy began developing a multi-mission aircraft capable of performing air-to-air and air-to-ground missions. The desire was to replace the F-4 Phantom and the A-7 Corsair.

The F/A-18 Hornet completed its first flight in 1978 and entered operational service with the Marine Corps in 1983 and the US Navy in 1984. By 1985, this new aircraft made its first deployment aboard the USS Constellation (CV-64).

Two Hornets flying

Photo: US Navy

The F/A-18 Super Hornet entered the fleet in 1999 as the replacement for the F-14 Tomcat. The original Hornet, while an incredible aircraft, was limited in range. Thus, the Super Hornet boasts a 20-percent larger airframe. This gave the aircraft increased lift and 33% more internal fuel capacity, increasing its mission range by 41%.

The Super Hornet is now manufactured by Boeing following its merger with McDonnell Douglas in 1997.

Technical notes for the F/A-18 Super Hornet, E and F models

General Specifications

Related Data

Primary Function

Multi-role attack and fighter aircraft.

Contractor

McDonnell Douglas (now The Boeing Company)

Unit Cost

$67.4 million (FY21)

Propulsion

Two F414-GE-400 turbofan engines. 22,000 pounds (9,977 kg) static thrust per engine

Length

60.3 feet (18.5 meters)

Height

16 feet (4.87 meters)

Wingspan

44.9 feet (13.68 meters)

Weight

Maximum Take Off Gross Weight is 66,000 pounds (29,932 kg)

Airspeed

Mach 1.8+

Ceiling

50,000+ feet

Range

Combat: 1,275 nautical miles (2,346 kilometers), clean plus two AIM-9s

Ferry

1,660 nautical miles (3,054 kilometers), two AIM-9s, three 480 gallon tanks retained.

Crew

A, C and E models: One B, D and F models: Two

Armament

One M61A1/A2 Vulcan 20mm cannon; AIM 9 Sidewinder, AIM-9X (projected), AIM 7 Sparrow, AIM-120 AMRAAM, Harpoon, Harm, SLAM, SLAM-ER (projected), Maverick missiles; Joint Stand-Off Weapon (JSOW); Joint Direct Attack Munition (JDAM); Data Link Pod; Paveway Laser Guided Bomb; various general purpose bombs, mines and rockets.

Recently, the Texan II has been successful in the Asian market, as Japan has agreed to purchase the aircraft for its air force’s pilot training program.

In addition to the increased fuel storage, the Navy ensured that the

Super Hornet
was equipped with two General Electric F414-GE-400 engines. These engines have a thrust class of 22,000 lb., compared to the F/A-18s earlier model F404-GE-102/103/402 engines, which fell into the 17,700 lb. thrust class. The new F414 engines drastically enhanced the Super Hornets’ performance, particularly while engaging in carrier operations.

F/A-18E Super Hornet

Photo: US Navy

With all of its enhancements, the Super Hornet can accomplish a wide spectrum of missions. These include air superiority, fighter escort, aerial refueling, electronic warfare (EA-18G Growler), reconnaissance, close air support, and day or night precision strike.

The first operational deployment of the Super Hornet, F/A-18E, was with VFA-115 aboard the USS Abraham Lincoln (CVN 72) in 2002. Initial combat action occurred in November of that same year when VFA-115 engaged in a strike on hostile targets in the “no-fly” zone in Iraq.

The T-6B Texan II

Inventory: 294 with 29 on order

The Texan II is a joint Air Force/Navy undergraduate pilot training aircraft. Developed for the aircraft was initiated under the Joint Primary Aircraft Training System program, with initial acquisition and support contracts being awarded in 1996.

The first operational Texan II landed at Randolph Air Force Base (AFB), Texas, in May 2000, with full-rate production being awarded in December 2001. Production of the aircraft for the Air Force was completed in 2010.

T-6B Texan flying

Photo: US Navy

This aircraft is based on the Swiss-designed Pilatus PC-9, and the Navy’s designation is the T-6B.

Randolph AFB, built between 1928 and 1930, has been a dedicated flight training school. Amongst other units, Randolph is home the Headquarters Air Education and Training Command, with the host unit being the 12th Flying Training Wing.

Technical notes for the T-6B Texan II

General Characteristics

Related Data

Primary Function

All-purpose jet trainer

Contractor

Hawker Beechcraft Aircraft Company

Date Deployed

First flight, July 2009; Operational, 2010

Propulsion

One Pratt & Whitney Canada PT-6A-68 turboprop engine; 1,100 horsepower

Length

33.3 feet (10.12 meters)

Height

10.8 feet (3.29 meters)

Wingspan

33.4 feet (10.18 meters)

Weight

Empty, 5,850 pounds (2,653.52 kg.); maximum takeoff weight, 6,900 pounds (3,129.79 kg)

Airspeed

270 knots at 1,000 feet level flight

Ceiling

31,000 feet (9,448.8 meters)

Range

Maximum, 900 nautical miles (1,666.8 km)

Crew

Two (instructor pilot, student pilot)

Armament

None

The Texan II is equipped with a Pratt & Whittney Canada PT6A turboprop engine that produces 1,100 horsepower. Because of its excellent thrust-to-weight ratio, the aircraft is capable of performing an initial climb of 3,100 feet per minute and can reach 18,000 feet in under six minutes.

Earlier this year, the Navy released a request for information regarding a replacement for the F-45.

A T-6B Texan about to take off

Photo: US Navy

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5 Fast Facts On The T-6 Texan II US Air Force Trainer

The moniker “Texan” is a proud name in U.S. Air Force Pilot and Naval Aviator training. The Texan II has been carrying on the name since 2001.

Recently, the Texan II has been successful in the Asian market, as Japan has agreed to purchase the aircraft and associated ground equipment for its air force’s pilot training program. Additionally, Vietnam and Thailand are set to purchase 12 Texan IIs.

The T-45 Goshawk

Inventory: 189 (The US is the primary user, but the UK also uses this aircraft)

The T-45 aircraft is the US Navy version of the British Aerospace Hawk aircraft, and became operational in 1991. It was designed for use in the intermediate and advanced portions of the Navy and Marine Corps pilot training program. The T-45 is specifically tailored for pilots who will deploy aboard an aircraft carrier and for practicing tactical strike missions.

T-45 Goshhawk on an aircraft carrier

Photo: US Navy | Petty Officer 2nd Class Bryan Mai

The current model, T-45C features a digital cockpit design.

Technical notes for the T-45 Goshawk

General Characteristics

Related Data

Primary Function

Training platform for Navy/Marine Corps pilots

Contractor

Boeing Company

Date Deployed

First flight, April 1988; Operational, 1991

Unit Cost

$17.2 million

Propulsion

Rolls Royce F405-RR-401 turbofan engine with 5,527 pounds thrust

Length

39 feet 4 inches (11.98 meters)

Height

13 feet 6 inches (4.11 meters)

Wingspan

30 feet 10 inches (9.39 meters)

Weight

Empty: 9,394 pounds (4,261 kg); maximum take-off: 13,500 pounds (6,075 kg)

Airspeed

645 miles per hour (1038 km per hour)

Ceiling

42,500 feet

Range

700 nautical miles (805 statute miles, 1288 km)

Crew

Two (instructor pilot, student pilot)

Armament

None, with the exception of trianing purposes

The T-45 is powered by a Rolls-Royce/Turbomeca Adour turbofan engine, which produces 5,200 pounds of thrust. The aircraft was engineered with a compact, low-wing configuration, with the instructor seated in an elevated position behind the student, under a large, single-piece, side-opening canopy.

T-45 Goshhawk preparing to land on an aircraft carrier

Photo: US Department of Defense

With regard to weapons training, the T-45 features five external storage stations, which can accommodate a wide array of weapons. This includes a 30mm gun pod capable of being mounted on the fuselage centerline station.

The first Growler to be produced left the shop floor on June 3, 2008.

Earlier this year, the Navy released a request for information regarding a replacement for the F-45. Candidates for the program are the Leonardo-Textron M-346N, the Boeing-Saab T-7, and the Lockheed Martin-KAI T-50.

EA-18G Growler

Inventory: 153

The Growler is a variant in the F/A-18 family of aircraft; it pairs the renowned Super Hornet platform with a sophisticated electronic warfare suite. The Growler is the first newly-designed electronic warfare aircraft produced in over 35 years. The reason behind its design and production was to replace the EA-6B Prowler.

E/A-18G Growler flying

Photo: US Navy

Electronic warfare features

  • ALQ-99 tactical jamming pods
  • AN/ALQ-249, the Next Generation Jamming Pod
  • ALQ-227 Communication Countermeasures Set

Related

How The US Navy Trains EA-18G Growler Pilots

US Navy pilots go through various training schools, each more difficult than the last.

Technical notes for the EA-18G Growler

General Characteristics

Related Data

Primary Function

Airborne Electronic Attack (AEA)

Contractor

The Boeing Company

Unit Cost

$67 million

Propulsion

Two F414-GE-400 turbofan engines. 22,000 pounds (9,977 kg) static thrust per engine

Length

60.2 feet (18.5 meters)

Height

16 feet (4.87 meters)

Wingspan

44.9 feet (13.68 meters)

Weight

Weight empty: 33,094 pounds; Recovery weight: 48,000 pounds

Ceiling

50,000 feet

Range

Combat: 850+ nautical miles with two AIM-120, three ALQ-99, two AGM-88 HARM, two 480 gallon external fuel tanks

Crew

2

Armament

Two AIM-120, two AGM-88 HARM, three ALQ-99

The first Growler to be produced left the shop floor on June 3, 2008. It was delivered to Electronic Attack Squadron (VAQ) 129, the Growler Fleet Replacement Squadron, at Naval Air Station (NAS) Whidbey Island in Washington.

Rather than design an entirely new aircraft, the Navy opted to base the Poseidon on the Boeing 737-800 commercial airliner fuselage.

Shortly after its first delivery, the Growler entered initial operational capability and full-rate production in the fall of 2009. By 2010, three squadrons, VAQ-132, VAQ-141, and VAQ-138, made the move from the Prowler to the Growler and were subsequently declared safe-for-flight.

EA-18G landing

Photo: US Navy

The Growler engaged in its first combat action in 2011 during Operation Odyssey Dawn in Libya.

All the Navy’s EA-18G squadrons are stationed at NAS

Whidbey Island
, except for VAQ-141, which is attached to Carrier Air Wing 5, based at Marine Corps Air Station Iwakuni, Japan.

P-8 Poseidon

Inventory: 118 with 10 on order

The Poseidon is a multi-mission aircraft developed to replace the P-3C Orion, which entered service with the Navy in the 1960s. It is tailored to provide long-range patrol services over maritime environments. In addition to surface surveillance, it scans below the surface for subsurface threats.

Poseidon

Photo: US Navy

Rather than design an entirely new aircraft, the Navy opted to base the Poseidon on the Boeing 737-800 commercial airliner fuselage. To prepare the aircraft for military service, they were substantially modified with a weapons bay, hard points, increased electrical generation, Boeing 737-900 wings, and further structural strengthening for military operations.

The Poseidon’s sensor suite

  • Active multi-static sensor system
  • Passive acoustic sensor system
  • Inverse synthetic aperture radar
  • Electronic support measures system
  • Electro-optical/infrared sensor
  • Digital magnetic anomaly detector

Technical notes for the P-8 Poseidon

General Characteristics

Related Data

Primary Function

Anti-Submarine Warfare (ASW) and Anti-surface Warfare (ASuW), Intelligence, Surveillance and Reconnaissance (ISR)

Contractor

Boeing Defense, Space and Security

Propulsion

2 CFM 56-7B engines with 27,300 lbs. thrust each

Length

129.5 feet (39.47 meters)

Height

42.1 feet (12.83 meters)

Wingspan

123.6 feet (37.64 meters)

Weight

Maximum gross takeoff, 189,200 pounds (85,820 kilograms)

Crew

Nine

Poseidon

Photo: US Navy 

Currently, there are more than 169 Poseidon’s in service with the US Navy and partner states around the world. Across the fleet, the Poseidon has racked up over 600,000 flight hours globally, and each aircraft is engineered for 25 years or 25,000 flight hours in the harshest maritime flight environments.

Related

Boeing’s P-8 Poseidon: What Weapons Are On Board?

The aircraft features 11 internal and external hardpoints for weapons.

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