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Handley Page Hermes

From Wikipedia, the free encyclopedia
Civilian airliner

HP.81 Hermes
Hermes IV of Air Safaris atManchester Airport in 1961
General information
TypeAirliner
ManufacturerHandley Page
Primary userBOAC
Number built29
History
Manufactured1945–1951
Introduction date6 August 1950
First flight2 December 1945
Retired1965
Developed fromHandley Page Hastings

TheHandley Page HP.81 Hermes was a civilianairliner designed and produced by theBritish aircraft manufacturerHandley Page.

The Hermes was developed during the 1940s in parallel with the closely relatedHandley Page Hastings military transport. It was a low-wingmonoplane, with most examples being powered by fourpiston engines. Originally intended to enter service in advance of the Hastings, development of the Hermes was delayed by the fatal loss of the first prototype during itsmaiden flight on 2 December 1945. Measures were taken to improve the airliner's stability as well as to expand its capacity, which sufficiently impressed theBritish Overseas Airways Corporation (BOAC) into placing a sizeable order for 25HP 81 Hermes IV on 4 February 1947. A pair ofturboprop-powered development aircraft were also ordered by theMinistry of Supply for experimental flights.

The Hermes entered airline service on 6 August 1950, having been delayed by roughly one year due to initial production aircraft being overweight. They would be operated by BOAC, the most prominent operator of the type, for less than a decade before they were sold onto other operators largely due to the rapid advances in airliners made during this era. During its later years of service, second hand Hermes were routinely used by variouscharter airlines. The final Hermes flight was performed sometime during 1969, by which point most of the type had already been scrapped as obsolete. A single example has been partially preserved.

Design and development

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Background

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The Hermes can be traced back to discussions held by theAir Staff (United Kingdom) as early as summer 1943.[1] At the time, authorities were considering not only the need for an immediate successor to theRoyal Air Force's (RAF) fleet ofHandley Page Halifax in the transport/freighter capacity, but also the role of an interim civil airliner for thepost-war years. Accordingly, during December 1944, priority orders were placed for various projects, including both the military and civil programmes proposed by the British aircraft manufacturerHandley Page.[1] For the civil airliner,Specification 15/43 was issued by theAir Ministry; this called for apressurised civil transport that was capable of carrying up to 34 first class or 50 tourist class passengers.[1]

During April 1944, at the urging ofGeorge Volkert, Handley Page's chief designer, to settle production priorities, the company's founder and managing directorFrederick Handley Page decided to merge the work of several projects and prioritise the transport aircraft; this also aligned with the release ofSpecification C.3/44, which sought a multipurpose transport.[2] Handley Page's proposal was accepted with no meaningful alterations sought. Shortly thereafter, it was recognised that development of the civil transport posed less of a challenge than the military transport project, thus it was decided that the airliner programme would be flown first.[3] The military transport aircraft, which would share a relatively high level of similarities with the civil project, would enter service as theHandley Page Hastings, while the civil transport became known as the Hermes.[4][5]

Despite the intentional similarities, there were distinct design differences between the two aircraft. Unlike thetailwheel of the Hastings, the Hermes was planned to have a nosewheellanding gear, although the first twoprototypes were completed with atailwheel undercarriage.[5] Despite the differences, both aircraft remained similar enough that they were produced using the same primary assemblyjigs. The first prototype was effectively an unpressurised "bare shell", while the second featured apressurised cabin and was fully equipped in most respects.[5] On 9 November 1945, a mock-up conference was held at the company'sCricklewood facility, attended by various airline officials and industry figures. Rapid progress on the first prototype's construction enabled it to commence ground trials atRadlett on 1 December 1945.[6]

Into flight and redesign

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While Handley Page had intended for the Hermes to be introduced in advance of the Hastings from an early stage of development, a delay to its production was necessitated after the first prototype (HP 68 Hermes 1), registeredG-AGSS, crashed during itsmaiden flight shortly after takeoff on 2 December 1945.[6] It is believed that the aircraft had encountered severe longitudinal instability due toelevator overbalance. Handley Page's chief test pilot and the chief test observer were both killed in the incident, while the prototype was completely destroyed by a post-impact fire.[7]

In order to sufficiently resolve the instability that caused the fatal crash, development of the civil Hermes was protracted, while work on the Hastings progressed more smoothly.[8] This delay presented the opportunity to undertake design revisions and improvements; it was decided that the second prototype's length would be extended to produce the HP 74 Hermes II. The prospects of powering the type withturboprop engines was also investigated around this time, but ultimately decided against.[9] The first Hermes II (G-AGUB) performed its first flight on 2 September 1947; it quickly proved to not only have greater stability, but to also possess a superior lift coefficient to the Hastings as well. On 4 September 1948, the type received itscertificate of airworthiness, clearing it for service.[4][10]

On 4 February 1947, firm orders were placed by theBritish Overseas Airways Corporation (BOAC) for 25 of the definitiveHP 81 Hermes IV. This model was furnished with atricycle undercarriage and powered by fourBristol Herculesradial engines, each capable of generating up to 2,100 hp (1,570 kW).[11] Additionally, a pair ofHermes V airliners were also ordered, the primary difference of this model was the use of fourBristol Theseus turboprop engines instead. Further turboprop-powered developments of the Hermes were also proposed to potential customers as a competitor to types such as theBristol Britannia.[11]

Operational history

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Airline operations

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BOAC Hermes IV atLondon Heathrow in 1953
Hermes IV ofBritavia atBlackbushe Airport in 1954

Despite the first Hermes IV (registeredG-AKFP) performing its first flight relatively quickly on 5 September 1948,[4] and quantity production being promptly established, BOAC was somewhat unsatisfied by the airliner, primarily due to the early aircraft being overweight.[12] This was in part due to the use of Hastings components and ad-hoc modifications to accelerate flight trials; it was promptly agreed that weight-saving modifications were to be made prior to BOAC issuing its final acceptance of the Hermes. Design alterations to reduce weight included the adoption of lighter floor members.[13]

On 6 August 1950, the Hermes IV finally entered service with BOAC, taking over from theAvro York on the West Africa service from London Heathrow toAccra viaTripoli,Kano andLagos, with services toKenya andSouth Africa commencing before the end of the year.[14][15] The Hermes IV was used by BOAC on routes to West and SouthAfrica. They were quickly replaced, however by the reliableCanadair Argonaut in 1952, although some re-entered service in July 1954 following the grounding of thede Havilland Comet, being retired again in December.[16][17]

This was not the end of the Hermes in airline service, however, as surplus aircraft were sold to independentcharter airlines, withAirwork purchasing four in 1952, others being operated byBritavia andSkyways, particularly in the trooping role.[18] Many of these aircraft were fitted with Hercules 773 engines, which could be operated on loweroctane fuel than the original Hercules 763s, being designated as Hermes IVA. They returned to Hermes IV standards when fuel supplies improved.[18][19]

Later, the Hermes were flown on inclusive tour holiday flights from the UK. The last operational civil Hermes,G-ALDA, flown by Air Links Limited, was retired on 13 December 1964, and was scrapped nine days later.[20][21]

Development aircraft

[edit]
Hermes V G-ALEU at the Farnborough SBAC show in 1950. Note the slimmer nacelles of the Theseus turboprop engines

The two turboprop Hermes V were owned by theMinistry of Supply and made their first flights in August 1949.[22] They were used for development of theBristol Theseus turboprop engine. The first aircraft was lost in a wheels-up landing atChilbolton airfield on 10 April 1951, but the second continued development flying with theAeroplane and Armament Experimental Establishment (A&AEE) atMOD Boscombe Down and theRoyal Aircraft Establishment (RAE) atFarnborough Airport until its retirement during September 1953.[23]

The prototype Hermes II was given military markings in October 1953 asVX234 and was used for various research and development programmes, including the testing of airborne radar for theRoyal Radar Establishment atRAF Defford, Worcestershire. It was finally retired in 1969, at which point the aircraft had been the final Hermes in operation.[24]

Preservation

[edit]

The fuselage of a Hermes IV (the formerBOAC aircraft G-ALDG namedHorsa) is preserved at theImperial War Museum Duxford.[25]

Variants

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All 29 aircraft were built atRadlett Aerodrome,Hertfordshire,England.

HP.68 Hermes I
Prototype powered by four 1,650 hp (1,230 kW)Bristol Hercules 101 radial engines. One built.
HP.74 Hermes II
Prototype powered by four 1,675 hp (1,249 kW)Bristol Hercules 121 engines and a 13 ft (4.57 m) longer forward fuselage. One built.
HP.81 Hermes IV
Production aircraft with tricycle landing gear, powered by four 2,100 hp (1,570 kW)Bristol Hercules 763 engines. Twenty-five built.
HP.81 Hermes IVa
Hermes IV modified to use 100-octane fuel, with the engine redesignated Hercules 773. Most converted back to Hermes IV standard.
HP.82 Hermes V
Development aircraft with four 2,490 hp (1,860 kW)Bristol Theseus 502 turboprops. Two built.

Operators

[edit]
AnAir Links Hermes atGatwick Airport, circa 1962
Preserved fuselage ofG-ALDG, at theImperial War Museum Duxford, 2010
 Bahamas
 Kuwait
 Lebanon
 United Kingdom

Accidents and incidents

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  • 3 December 1945 - Hermes IG-AGSS the prototype Hermes crashed on the first test flight soon after takeoff three miles from Radlett Aerodrome. The two Handley Page test pilots were killed.
  • 26 May 1952 - Hermes IVG-ALDN (Horus), operated by BOAC, en route fromTripoli, Libya, toKano, Nigeria, flew off course for several hours and ran out of fuel, force landing in theSahara Desert south ofAtar, Mauritania. The passengers and crew all survived and spent several days in the desert before making their way to an oasis, where First Officer Ted Haslam, who had suffered a head injury in the crash, died.[26][27][28]
  • 25 August 1952 - Hermes IV 'G-ALDF' operated by Air-work Ltd en route from Blackbushe to Khartoum via Malta, ditched off Sicily (near Trapani) at 0300 LT, following failure of two engines and the prospect of the other two engines failing. Electrical power also failed, so no lights or radio available. The ditching was "brilliantly performed" and successful, but 6 passengers (including 4 young children) and one air hostess drowned, mainly due to defective life jackets and lack of a life raft for the children. Investigation report by the Italian authorities (not published in UK) is summarised in ICAO Circular 38-AN/33.[29] Contains some criticism of the crew and operating company and recommended improvements to the aircraft and to safety provisions. Matter raised in Parliament by Wedgwood Benn MP.[30]
  • 4 March 1956 - Hermes IVG-ALDW operated by Skyways Limited was destroyed on the ground by a time-bomb in the forward freight compartment. The aircraft was atNicosia Airport, Cyprus when the explosion occurred 20 minutes before the aircraft was due to depart for the United Kingdom with 68 passengers.[31] There were no fatalities.[32]
  • 5 August 1956 - Hermes IVG-ALDK operated by Britavia suffered the collapse of the nose undercarriage atDrigh Road Airport,Karachi,Pakistan. The aircraft was damaged beyond economic repair.[33]
  • 5 November 1956 - Hermes IVaG-ALDJ operated by Britavia crashed on night approach toBlackbushe Aerodrome,England in bad weather. Seven of the 80 occupants died.[34]
  • 1 April 1958 - Hermes IVG-ALDV operated by Skyways Limited. Crashed at Meesden Green, close to Stansted Airport, whilst on an airtest after an engine change. The crew of three, Capt. Rayment, Capt. West and FE. N Bradley were all killed.
  • 9 October 1960 - Hermes IVG-ALDC ofFalcon Airways overran the runway on landing atSouthend Airport, ending up across theShenfield to Southend railway line. The aircraft was written off but all 76 people on board survived.[35]

Specifications (Hermes IV)

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Hermes IV

Data fromJane's All the World's Aircraft 1950-51[36]

General characteristics

  • Crew: Five flight crew, plus cabin crew
  • Capacity: 40 - 82 passengers
  • Length: 96 ft 10 in (29.51 m)
  • Wingspan: 113 ft (34 m)
  • Height: 29 ft 11 in (9.12 m)
  • Wing area: 1,408 sq ft (130.8 m2)
  • Airfoil:root:NACA 23021;tip:NACA 23007[37]
  • Empty weight: 55,350 lb (25,106 kg) basic equipped
  • Max takeoff weight: 82,000 lb (37,195 kg)
  • Maximum landing weight: 75,000 lb (34,019 kg)
  • Fuel capacity: 3,224 imp gal (3,872 US gal; 14,657 L) in integral wing tanks ; 4x 37 imp gal (44 US gal; 168 L) oil tanks
  • Powerplant: 4 ×Bristol Hercules 14-cylinder air-cooled radial piston engines, 2,020 hp (1,510 kW) each for take-off
  • Propellers: 4-bladedde Havilland Hydromatic, 13 ft (4.0 m) diameter constant-speed fully-feathering reversible-pitch propellers

Performance

  • Maximum speed: 357 mph (575 km/h, 310 kn) at 20,000 ft (6,100 m)
  • Cruise speed: 266 mph (428 km/h, 231 kn) maximum weak mixture at 10,000 ft (3,000 m)
274 mph (238 kn; 441 km/h) maximum weak mixture at 20,000 ft (6,100 m)
213 mph (185 kn; 343 km/h) maximum range speed at 10,000 ft (3,000 m)
244 mph (212 kn; 393 km/h) maximum range speed at 20,000 ft (6,100 m)
  • Range: 3,147–3,554 mi (5,065–5,720 km, 2,735–3,088 nmi) with 2,213 lb (1,004 kg) payload at 20,000 ft (6,100 m) dependent on speed
  • Service ceiling: 24,500 ft (7,500 m)
  • Rate of climb: 1,030 ft/min (5.2 m/s)
  • Time to altitude:
  • 10,000 ft (3,000 m) in 10 minutes 30 seconds
  • 20,000 ft (6,100 m) in 25 minutes
  • Wing loading: 58.2 lb/sq ft (284 kg/m2)
  • Power/mass: 0.104 hp/lb (0.171 kW/kg)
  • Take-off run: 3,330 ft (1,015 m) at 82,000 lb (37,195 kg)
  • Take-off distance to 50 ft (15 m): 4,440 ft (1,350 m)
  • Landing distance from 50 ft (15 m): 4,224 ft (1,287 m)

See also

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Related development

Aircraft of comparable role, configuration, and era

References

[edit]

Citations

[edit]
  1. ^abcBarnes 1976, p. 435.
  2. ^Barnes 1976, pp. 435-436.
  3. ^Barnes 1976, p. 436.
  4. ^abcJackson 1973, p. 247.
  5. ^abcBarnes 1976, pp. 436–437.
  6. ^abBarnes 1976, p. 437.
  7. ^"Loss of the prototype Hermes"Flight 6 December 1945.
  8. ^Barnes 1976, pp. 437–438.
  9. ^Barnes 1976, p. 460.
  10. ^Barnes 1976, p. 462.
  11. ^abBarnes 1976, pp. 460-461.
  12. ^Barnes 1976, p. 465.
  13. ^Barnes 1976, pp. 465-466.
  14. ^Jackson 1973, pp. 248–249.
  15. ^Barnes 1976, p. 466.
  16. ^Jackson 1973, p. 249.
  17. ^Barnes 1976, p. 471.
  18. ^abJackson 1973, pp. 249–250.
  19. ^Barnes 1976, pp. 471-472.
  20. ^Jackson 1973, p. 251.
  21. ^Barnes 1976, p. 472.
  22. ^Barnes 1976, pp. 464, 466.
  23. ^Barnes 1976, pp. 466-467, 469.
  24. ^Barnes 1976, pp. 472–474.
  25. ^"Handley Page Hermes IV (Fuselage)". britairliners.org. Retrieved28 September 2021.
  26. ^Fisher, John Hayes (Producer). (2003). Desert Rescue [Television series episode]. InMeet the ancestors. London: British Broadcasting Corporation.
  27. ^Magna, April 2014, the magazine of the Friends of The National Archives, London.
  28. ^Lost in the Sahara atIMDb Edit this at Wikidata
  29. ^ baaa-acro.com/sites/default/files/import/uploads/2017
  30. ^Benn, Wedgwood (19 November 1953), "Aircraft crash, Sicily (Report)",House of Commons Paper, Series 5, vol. 520, UK Parliament, p. 1965
  31. ^"Civil Aviation: Hermes Sabotage".Flight. 16 March 1956, p.306.
  32. ^"ASN Aircraft accident Handley Page HP.81 Hermes IV G-ALDW Nicosia". Aviation Safety Network. 26 October 2014. Retrieved26 October 2014.
  33. ^Chesterfield, Lyn. "Hermes prang".Aeroplane. No. January 2011. Kelsey Publishing. p. 82.
  34. ^ICAO Accident Digest No.8, Circular 54-AN/49 (138–147)
  35. ^"G-ALDC Accident description". Aviation Safety Network. Retrieved22 March 2011.
  36. ^Bridgman, Leonard, ed. (1950).Jane's All the World's Aircraft 1950-51. London: Sampson Low, Marston & Co. p. 65c.
  37. ^Lednicer, David."The Incomplete Guide to Airfoil Usage".m-selig.ae.illinois.edu. Retrieved16 April 2019.

Bibliography

[edit]
  • Barnes, C. H.Handley Page Aircraft Since 1907. London: Putnam, 1976.ISBN 0-370-00030-7.
  • Barnes, C. H.Handley Page Aircraft Since 1907. London: Putnam & Company, Ltd., 1987.ISBN 0-85177-803-8.
  • Clayton, Donald C.Handley Page, an Aircraft Album. Shepperton, Surrey, UK: Ian Allan Ltd., 1969.ISBN 0-7110-0094-8.
  • Jackson, A.J.British Civil Aircraft since 1919: Volume 2. London:Putnam, Second edition 1973.ISBN 0-370-10010-7.

Further reading

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  • Donald, David (1997).The encyclopedia of world aircraft (Updated ed.). Leicester: Blitz Editions. p. 496.ISBN 1-85605-375-X.

External links

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