AV-8B (NA)
This page is about the American jet fighter AV-8B (NA). For other versions, see Harrier (Family). |
Contents
Description
General info
Flight performance
Characteristics | Max Speed (km/h at 0 m - sea level) |
Max altitude (metres) |
Turn time (seconds) |
Rate of climb (metres/second) |
Take-off run (metres) | |||
---|---|---|---|---|---|---|---|---|
AB | RB | AB | RB | AB | RB | |||
Stock | 1,151 | 1,145 | 12192 | 32.2 | 33.1 | 81.7 | 75.2 | 550 |
Upgraded | 1,164 | 1,156 | 31.7 | 32.0 | 102.7 | 87.0 |
Details
Features | |||||
---|---|---|---|---|---|
Combat flaps | Take-off flaps | Landing flaps | Air brakes | Arrestor gear | Drogue chute |
X | ✓ | ✓ | ✓ | X | X |
Limits | ||||||
---|---|---|---|---|---|---|
Wings (km/h) | Gear (km/h) | Flaps (km/h) | Max Static G | |||
Combat | Take-off | Landing | + | - | ||
0 | 648 | N/A | 828 | 556 | ~14 | ~6 |
Optimal velocities (km/h) | |||
---|---|---|---|
Ailerons | Rudder | Elevators | Radiator |
< 648 | < 950 | < 790 | N/A |
Engine performance
Engine | Aircraft mass | ||||||
---|---|---|---|---|---|---|---|
Engine name | Number | Basic mass | Wing loading (full fuel) | ||||
Rolls-Royce F402-RR-401 | 1 | 5,918 kg | 439 kg/m2 | ||||
Engine characteristics | Mass with fuel (no weapons load) | Max Takeoff Weight | |||||
Weight (each) | Type | 10m fuel | 20m fuel | 30m fuel | 34m fuel | ||
1,687 kg | Vectored-thrust low-bypass turbofan | 6,605 kg | 7,292 kg | 7,978 kg | 8,253 kg | 12,679 kg | |
Maximum engine thrust @ 0 m (RB/SB) | Thrust to weight ratio @ 0 m (WEP) | ||||||
Condition | 100% | WEP | 10m fuel | 20m fuel | 30m fuel | 34m fuel | MTOW |
Stationary | 9,071 kgf | 9,625 kgf | 1.46 | 1.32 | 1.21 | 1.17 | 0.76 |
Optimal | 9,071 kgf (0 km/h) |
9,625 kgf (0 km/h) |
1.46 | 1.32 | 1.21 | 1.17 | 0.76 |
The F402-RR-401 engine loses a significant amount of thrust as your speed increases |
Survivability and armour
Modifications and economy
Armaments
Ballistic Computer | |||
---|---|---|---|
CCIP (Guns) | CCIP (Rockets) | CCIP (Bombs) | CCRP (Bombs) |
Offensive armament
The AV-8B (NA) is armed with:
- 2 x 30 mm ADEN Mk.4 cannons, belly-mounted (130 rpg = 260 total)
Suspended armament
The AV-8B (NA) can be outfitted with the following ordnance:
1 | 2 | 3 | 4 | 5 | ||
---|---|---|---|---|---|---|
250 lb LDGP Mk 81 bombs | 1 | 1 | 1 | 1 | 1 | |
250 lb Mk 81 Snakeye bombs | 1 | 1 | 1 | 1 | 1 | |
500 lb LDGP Mk 82 bombs | 1 | 1 | 1 | 1 | 1 | |
500 lb Mk 82 Snakeye bombs | 1 | 1 | 1 | 1 | 1 | |
1,000 lb LDGP Mk 83 bombs | 1 | 1 | ||||
Mk 77 mod 4 incendiary bombs | 1 | 1 | 1 | 1 | 1 | |
FFAR Mighty Mouse rockets | 7, 19 | 7, 19 | 7, 19 | 7, 19 | ||
Zuni Mk32 Mod 0 ATAP rockets | 4 | 4 | 4 | 4 | ||
AIM-9G Sidewinder missiles | 1 | 1 | ||||
Countermeasures | 240 |
Default weapon presets | |
---|---|
|
Usage in battles
Pros and cons
Pros:
- Thrust vectoring capabilities
- Can be used during combat to temporarily boost turn rate
- Can land and rearm on the helicopter bases in combined battles
Cons:
- Heavy airframe loses significant speed in turns
- Limited WEP and lack of afterburner
- Engine overheats very quickly above 90% throttle
- Using thrust vectoring in combat bleeds speed and leaves you vulnerable
- Stiffens up in dives; this can be fatal during ground attack missions
History
The US military had been paying close attention to the development of British VTOL aircraft through the 1950s / 60s, taking part in the testing and evaluation of the Hawker Siddeley P.1127 / Kestrel FGA.1 (prototypes that would eventually develop into the Harrier) in the mid-1960s. At the 1968 Farnborough air show two United States Marine Corps (USMC) pilots, Col. Thomas H. Miller (eventually promoted to Lieutenant General) and Lt. Col. Bud Baker unexpectedly arrived at the Hawker Siddeley Aviation (HSA) chalet and announced they had been sent to test fly the new Harrier GR.1 aircraft. Within 2 weeks of the show both pilots had flown the Harrier and shortly after returned to the US with a very positive report of the aircraft.[1]
Within three months of the report a team of US test pilots were in the UK evaluating the Harrier and within a further five months the US had declared its intention to buy 110 Harriers by the mid 1970s. The US congress originally insisted that the Harriers should be built in the US, leading to HSA signing a 15 year agreement with McDonnell-Douglas, where McDonnell-Douglas would build the aircraft in the US and both parties would share data and designs of any aircraft related to the Harrier.[1] However later, after realizing the cost increase that would come from shifting production to the US, it was instead decided all 110 aircraft would be built by HSA in the UK. The aircraft would be purchased as "off the shelf" products with only limited modifications made from the Harrier GR.1. The US Harriers would have the more powerful Pegasus Mk 103 engine, the ability to carry two Sidewinder missiles, and other minor changes such as US radio equipment.[1]
The Harrier entered service with the USMC in 1971, under the designation AV-8A.[1]Marine Attack Squadron 513 (VMA-513) was the first squadron to receive its Harriers with VMA-231 and VMA-542 following. Shortly after it entered service the US decided to replace the British Ferranti FE 541 Inertial Navigation and Attack System (INAS) system with an American system known as "baseline". The FE 541 was an advanced system, it was able to use inertial navigation to plot the Harrier's location on a moving map in the cockpit and had various weapons aiming modes to allow for accurate bombing. The US however did not like the FE 541 finding it too complicated and difficult to maintain. In addition the FE 541 required a calibration process to be carried out before use, which could not be completed onboard a ship, severely limiting it's usefulness to the USMC. The baseline system was far simpler than the FE 541 and did not provide navigation functionality; with the removal of the large moving map display the USMC took the opportunity to change the layout of the AV-8A's cockpit making it different to that in British Harriers.[1]
Media
- Skins
See also
Links to the articles on the War Thunder Wiki that you think will be useful for the reader, for example:
- reference to the series of the aircraft;
- links to approximate analogues of other nations and research trees.
External links
References
- Citations
- Bibliography
- Fozard, J. (1978). The British Aerospace Harrier Case Study in Aircraft Design. American Institute of Aeronautics & Astronautics.
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