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Handley Page Hendon (HP.25)


Biplane Torpedo Bomber Prototype Aircraft [ 1924 ]



Just six prototypes made up the twin-seat Handley Page Hendon - developed from the earlier Hanley single-seat biplane - torpedo bomber program.



Authored By: Staff Writer | Last Edited: 01/31/2019 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.

GO TO SPECIFICATIONS [+]
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Part of the work completed by Handley Page during the early 1920s, in an attempt to satisfy a standing Fleet Air Arm (FAA) requirement of 1920 for a modern carrier-based torpedo bomber, was the "Hendon". This twin-seat torpedo-carrying biplane was built alongside the single-seat "Hanley" of similar form and function, both of which would ultimately be passed over for the Blackburn "Dart" (detailed elsewhere on this site). The Hendon was completed in six prototype examples and flown in 1924 but these ended their days as test aircraft for various wing surface control fittings and carrier operation evaluations.

The aircraft exhibited many qualities of the time: an over-under biplane wing configuration, open-air cockpit, and fixed tail-dragger undercarriage. The wings were multi-bayed with parallel struts and left unstaggered. The engine was positioned at the nose in the usual way and drove a two-bladed propeller. The cockpit was seated near midships with generally poor views for the pilot (the machine gunner was directly behind). The fuselage sported slab sides and tapered towards the tail to which a single-finned rudder was affixed. The undercarriage involved a twin-wheeled component under the forward mass of the aircraft with a simple tail skid under the rear.

FAA authorities saw enough value in the Hendon to order is as a test aeroplane through a contract given on November 27th, 1923 - this to cover a total of six aircraft. Hanley had designed this two-seater from the final Hanley form, the Hanley III. The Hanley III was the third of three iterations born from the Hanley project and ultimately rectified control issues in the design while incorporating full-span leading edge slots for low-altitude, low-speed handling crucial to carrier operations. Specification 25/23 was drawn up to cover the new aircraft, then known as the "Type Ta" (retrospectively redesignated to "HP.25").

A first-flight of the prototype Hendon was recorded on July 7th, 1924 and the entire lot was constructed before the end of the year for further testing. Some revisions were made to the design when the full war load was added, resulting in slight sweepback of the wing mainplanes to offset heavier loads placed on the tail section.

Three distinct variants of the Hendon were completed: Hendon I, Hendon II, and Hendon III. The Hendon II mark were three revised Hendon I aircraft with improved slot gear and the Hendon III was a one-off conversion of a Hendon II model with slotted flaps.

The basic approach to the design borrowed much from the Hanley save for a slightly lengthened fuselage to accommodate the second crewmember - as such a tandem-seat arrangement was used. Dimensions included a running length of 34.5 feet, a wingspan of 46 feet, and a height of 13.7 feet. Empty weight reached 4,350lb and the Maximum Take-Off Weight (MTOW) reached 7,000lb. Power was from a Napier Lion IIB 12-cylinder, water-cooled unit of 450 horsepower - the same engine featured in the earlier Hanley and the competing Dart aircraft - and this was used to power a two-bladed wooden propeller at the nose. Performance specs included a maximum speed of 110 miles-per-hour with a service ceiling up to 9,500 feet.

Standard armament was a single 0.303 Vickers Machine Gun over the nose in a fixed, forward-firing mounting synchronized to fire through the spinning propeller blades as well as a single 0.303 Lewis Machine Gun on a trainable mounting at the rear cockpit. The bombload was either a single 18" (457mm) aerial torpedo or 2 x 230lb drop bombs.©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
1924

Origin
United Kingdom national flag graphic
United Kingdom

Status
CANCELLED
Development Ended.
Crew
2

Production
6
UNITS


National flag of the United Kingdom United Kingdom (cancelled)
(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.
Maritime / Navy
Land-based or shipborne capability for operating over-water in various maritime-related roles while supported by allied naval surface elements.
X-Plane (Developmental, Prototype, Technology Demonstrator)
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.


Length
34.5 ft
(10.51 m)
Width/Span
45.9 ft
(14.00 m)
Height
13.7 ft
(4.17 m)
Empty Wgt
4,409 lb
(2,000 kg)
MTOW
6,967 lb
(3,160 kg)
Wgt Diff
+2,557 lb
(+1,160 kg)
(Showcased structural values pertain to the Handley Page Type Ta / HP.25 production variant)
Installed: 1 x Napier Lion IIB 12-cylinder water-cooled engine developing 450 horsepower and driving a two-bladed wooden propeller at the nose.
Max Speed
110 mph
(177 kph | 96 kts)
Ceiling
9,514 ft
(2,900 m | 2 mi)


♦ 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 Handley Page Type Ta / HP.25 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:
1 x 0.303 Vickers Machine Gun in fixed, forward-firing mounting over the nose and synchronized to fire through the spinning propeller blades.
1 x 0.303 Lewis Machine Gun on trainable mounting in rear cockpit.

OPTIONAL:
1 x 18" (457mm) aerial torpedo OR 2 x 230lb conventional drop bombs.


Supported Types


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


(Not all ordnance types may be represented in the showcase above)
Hardpoint Mountings: 3


"Hendon" - Base Series Name.
Hendon I - Initial prototype design based in the single-seat Hanley III torpedo carrier prototype; six examples completed as test aircraft under FAA contract.
Hendon II - Three Hendon III aircraft with modified leading edge wings.
Hendon III - One-off modification of Hendon II aircraft; slotted flaps added.


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Images Gallery



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Image of the Handley Page Hendon (HP.25)
Image from the Public Domain.


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