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Curtiss A-18 (Shrike II)


Ground Attack Aircraft [ 1936 ]



Limited to thirteen total examples, the Curtiss A-18 managed a short service life for the Americans and was replaced by more potent, advanced forms before the end.



Authored By: Staff Writer | Last Edited: 08/08/2018 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.

GO TO SPECIFICATIONS [+]
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In the mid-1930s, the United States Army Air Corps (USAAC) began evaluation of a new twin-engined, twin-seat ground attack aircraft through the Curtiss XA-14 program. The design offered a very modern appearance coupled with exceptional performance for its time, the latter quality allowing the aircraft to outpace even some of the fastest fighters of the period. One test article was completed and this led to the developmental Y1A-18 and, ultimately, the A-18 "Shrike" designation. However total production only ever reached 13 aircraft as the A-18 series was, itself, outpaced by newer designs - the A-18 never materialized into a long-term USAAC solution as it was quickly superseded by more advanced forms.

The ground attack aircraft had increasingly grown in tactical value for warplanners heading into World War 2 (1939-1945). These platforms offered about the same firepower as a medium-class bomber but could also be used in the direct-attack role as a heavy fighter. Such flexibility was highly sought after by air services of the time and the A-18 seemingly fit the bill for the USAAC as its revised its stock of aging aircraft. The service went on to evaluate a small collection of twin-engined, twin-seat types prior to the Grand War.

The A-18 held roots in the original Curtiss Model 76 which was outfitted with a pair of Wright XR-1510 "Whirlwind" radial piston engines of 600hp each and driving two-bladed propellers. A monoplane design form was selected with the engines held in streamlined nacelles along the wing leading edges. The wings and engines straddled the slim fuselage which was aerodynamically refined. The crew of two sat under a relatively long, framed canopy. The tail unit was of a traditional arrangement featuring a sole vertical fin and low-set horizontal planes. The undercarriage was of a typical tail-dragger configuration.

After testing with the Model 76, the aircraft was revised with Wright R-1670-5 "Cyclone" engines of 775 horsepower (each) and driving "constant speed" propellers to help increase performance. Testing resumed which produced evermore slightly evolved models which trialed engines and weapons (including fitting Wright R-1820-47 "Cyclone" radials of 850 horsepower each with three-bladed propellers; cannon calibers as large as 37mm were also tested). Before the end, the design had become the Model 76A ("Shrike II") which was the basis for the definitive A-18 service test form appearing in 1936.

A-18s were delivered to the 8th Attack Squadron, 3rd Attack Group (Barksdale Field, Louisiana) from July to October of 1937 and these teams quickly showcased the aircraft to be an effective gunnery and bombing platform (bombs were carried in compartments within each wing assembly). The A-18 was then used in training for 1940. Despite this showing, there lay several weakness in her design that revealed themselves with operational use. Her undercarriage was prone to collapsing when landing or taking off and her engines led to an underpowered aircraft which, in turn, limited its bomb load capabilities. To further hamper her future reach in service to the USAAC, the design was an expensive investment at about $105,000 USD per single unit. Curtiss attempted to rectify some of her issues including offering the product with Wright R-1830 radials but the damage was done.

Despite its potential at the outset, the operational life of the A-18 proved short as the 8th Attack Squadron moved on adopting the newer Douglas A-20 "Havoc" (detailed elsewhere on this site) from 1941 on. There was also little foreign interest in acquiring the aircraft which held design roots in the mid-1930s - this all but doomed any future the A-18 was expected to have. What few examples of the A-18 remained flew throughout 1942 but the line was completely retired in 1943. None saw combat action in World War 2 but two operated by way of the 108th Reconnaissance Squadron over the Panama Canal Zone where they saw their last days in the sky.

The A-18 proved instrumental to the USAAC observers as the value of larger, heavier twin-engined multi-crew systems had revealed itself. A-20s and Martin A-26 "Invaders" became some of the more classic forms of this aircraft type to see service in World War 2.©MilitaryFactory.com
Note: The above text is EXCLUSIVE to the site www.MilitaryFactory.com. It is the product of many hours of research and work made possible with the help of contributors, veterans, insiders, and topic specialists. If you happen upon this text anywhere else on the internet or in print, please let us know at MilitaryFactory AT gmail DOT com so that we may take appropriate action against the offender / offending site and continue to protect this original work.
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Specifications



Service Year
1936

Origin
United States national flag graphic
United States

Status
RETIRED
Not in Service.
Crew
2

Production
13
UNITS


Curtiss Aeroplane and Motor Company - USA
(View other Aviaton-Related Manufacturers)
National flag of the United States United States
(OPERATORS list includes past, present, and future operators when applicable)
Ground Attack (Bombing, Strafing)
Ability to conduct aerial bombing of ground targets by way of (but not limited to) guns, bombs, missiles, rockets, and the like.
Close-Air Support (CAS)
Developed to operate in close proximity to active ground elements by way of a broad array of air-to-ground ordnance and munitions options.


Length
41.0 ft
(12.50 m)
Width/Span
59.5 ft
(18.15 m)
Height
11.5 ft
(3.50 m)
Empty Wgt
9,414 lb
(4,270 kg)
MTOW
13,173 lb
(5,975 kg)
Wgt Diff
+3,759 lb
(+1,705 kg)
(Showcased structural values pertain to the base Curtiss A-18 (Shrike II) production variant)
Installed: 2 x Wright R-1820-47 air-cooled radial piston engines developing 850 horsepower each.
Max Speed
249 mph
(400 kph | 216 kts)
Ceiling
27,461 ft
(8,370 m | 5 mi)
Range
652 mi
(1,050 km | 1,945 nm)


♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030


(Showcased performance specifications pertain to the base Curtiss A-18 (Shrike II) production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
STANDARD:
4 x 0.30 caliber Browning M1919 machine guns in fixed, forward-firing positions.
1 x 0.30 caliber machine gun in rear defensive position

OPTIONAL:
Up to 400 lb of conventional drop bombs held in wing bays.
Up to 200 lb of conventional drop bombs held underwing


Supported Types


Graphical image of an aircraft medium machine gun
Graphical image of an aircraft conventional drop bomb munition


(Not all ordnance types may be represented in the showcase above)
Hardpoint Mountings: 2


A-18 "Shrike II" - Base Series Designation
YA-14 - Single prototype model
Y1A-18 - Developmental test forms
A-18 - Production model designation


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Image of the Curtiss A-18 (Shrike II)
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