Recent from talks
Handley Page Marathon
Knowledge base stats:
Talk channels stats:
Members stats:
Handley Page Marathon
The Handley Page (Reading) H.P.R.1 Marathon was a British four-engined civil transport aircraft, capable of seating up to 20 passengers. It was designed by Miles Aircraft Limited and largely manufactured by Handley Page (Reading) Limited (who acquired Miles' assets) at Woodley Aerodrome, Reading, England.
Originally submitted to the Air Ministry as a four-engined high-wing monoplane weighing roughly 16,500 lb, the concept was well received by the Brabazon Committee, with Miles being issued with instructions to proceed. While development proceeded, various agencies argued over the aircraft's specification, leading to multiple attempts to change the design midway though, delaying progress and inflating costs. Delays over the placement of a firm order contributed to Miles' bankruptcy, after which its assets were acquired by Handley Page and formed into the subsidiary Handley Page (Reading) Limited to produce the Marathon.
The Marathon represented several firsts, being Miles' first four engined aircraft as well as their first all-metal design; it was also recognised that the Marathon was the first British transport aircraft to comply with the stringent International Civil Aviation Organization (ICAO). However, the lack of commercial involvement in the specification to which the aircraft was built likely heavily contributed to the lukewarm response it received from such operators, with British European Airways (BEA) opting to not introduce the type despite buying seven of them with intentions of doing so. The largest operator of the Marathon was the Royal Air Force, where the type were primarily used as a navigation trainer.
The origins of the Marathon are closely associated with the opportunities offered by the Brabazon Committee, which sought to best direct the British aircraft industry's efforts for the postwar civilian market. Work on the project had commenced under Miles Aircraft Limited, having been originally envisioned as a four-engined low-wing cantilever monoplane that had been intended as a natural successor to the prewar de Havilland Express. Miles' management were convinced that there would be a sizable market for a larger aircraft, but there was some dispute as to how big it should be, with internal proposals ranging from 12,000 lb to 20,000 lb, while some designers pushed for the use of a pair of Bristol-built engines capable of 1,100 hp instead of four de Havilland Gipsy Queen engines producing 330 hp. It was decided to compromise on a four-engined aircraft with a high-mounted wing that weighed roughly 16,500 lb; this proposal was submitted to the Air Ministry for review, resulting in Specification 18/44 being written to fit it.
While the concept quickly received the Brabazon Committee's approval, who assigned it the designation Type 5a, Miles did not receive a direct contract immediately; instead, the specification was released to competitive tender during May 1944. While rival bids were submitted from companies such as Percival and Armstrong Whitworth, Miles' design was selected as the winner, with the company being issued an instruction to proceed with development during October 1944. As per the convention at the time, development and ordering were overseen by the Air Ministry alone, with Miles being forbidden from directly communicating with commercial operators to seek input on their requirements or suggestions.
By April 1945, the majority of the design features for the aircraft, which was designated M.60 Marathon, had been agreed upon. The Marathon incorporated numerous modern features, including its all-metal construction, being the first Miles-built aircraft to be built as such, as well as being the company's first four-engined design. Around this latter stage of development, work was protracted by a multitude of state agencies becoming involved and pushing for their own diverse requirements to be incorporated, some of which were contradictory and occasionally impractical to achieve, such as the use of a pressurised cabin or a very high level of structural strength. This led to numerous disputes over which groups had authority to overrule one another and led to considerable resource waste on the project.
A total of three prototypes were built for the development process, the first of which performed the type's maiden flight on 19 May 1946. Flight testing of the Marathon yielded positive results from the onset; during its official trials, the aircraft was described as being the nicest multi-engined aeroplane to have ever been handled by its test pilots. It was also recognised that the Marathon was the first British transport aircraft to comply with the stringent International Civil Aviation Organization (ICAO) safety requirements. However, on 10 May 1948, tragedy struck when one of the prototypes was lost during official trials held at RAF Boscombe Down; the loss was attributed to pilot error, having failed to adjust the fins to their normal position, resulting in mid-flight structural failure.
While Miles had worked on the Marathon under its instructions to proceed, the issuing of a production contract by British authorities was anything but prompt. The second prototype was in flight and the third was at an advanced stage before negotiations towards such a contract were successful, but by then it was too late for the company. Miles had experienced persistent financial difficulties and was banking on at least 100 Marathons being ordered; however, the initial production contract that emerged only ordered 50 aircraft, of which 30 were intended for British European Airways (BEA) while 20 were directed to British Overseas Airways Corporation (BOAC), which already intended to resell its aircraft onto other airlines.
Hub AI
Handley Page Marathon AI simulator
(@Handley Page Marathon_simulator)
Handley Page Marathon
The Handley Page (Reading) H.P.R.1 Marathon was a British four-engined civil transport aircraft, capable of seating up to 20 passengers. It was designed by Miles Aircraft Limited and largely manufactured by Handley Page (Reading) Limited (who acquired Miles' assets) at Woodley Aerodrome, Reading, England.
Originally submitted to the Air Ministry as a four-engined high-wing monoplane weighing roughly 16,500 lb, the concept was well received by the Brabazon Committee, with Miles being issued with instructions to proceed. While development proceeded, various agencies argued over the aircraft's specification, leading to multiple attempts to change the design midway though, delaying progress and inflating costs. Delays over the placement of a firm order contributed to Miles' bankruptcy, after which its assets were acquired by Handley Page and formed into the subsidiary Handley Page (Reading) Limited to produce the Marathon.
The Marathon represented several firsts, being Miles' first four engined aircraft as well as their first all-metal design; it was also recognised that the Marathon was the first British transport aircraft to comply with the stringent International Civil Aviation Organization (ICAO). However, the lack of commercial involvement in the specification to which the aircraft was built likely heavily contributed to the lukewarm response it received from such operators, with British European Airways (BEA) opting to not introduce the type despite buying seven of them with intentions of doing so. The largest operator of the Marathon was the Royal Air Force, where the type were primarily used as a navigation trainer.
The origins of the Marathon are closely associated with the opportunities offered by the Brabazon Committee, which sought to best direct the British aircraft industry's efforts for the postwar civilian market. Work on the project had commenced under Miles Aircraft Limited, having been originally envisioned as a four-engined low-wing cantilever monoplane that had been intended as a natural successor to the prewar de Havilland Express. Miles' management were convinced that there would be a sizable market for a larger aircraft, but there was some dispute as to how big it should be, with internal proposals ranging from 12,000 lb to 20,000 lb, while some designers pushed for the use of a pair of Bristol-built engines capable of 1,100 hp instead of four de Havilland Gipsy Queen engines producing 330 hp. It was decided to compromise on a four-engined aircraft with a high-mounted wing that weighed roughly 16,500 lb; this proposal was submitted to the Air Ministry for review, resulting in Specification 18/44 being written to fit it.
While the concept quickly received the Brabazon Committee's approval, who assigned it the designation Type 5a, Miles did not receive a direct contract immediately; instead, the specification was released to competitive tender during May 1944. While rival bids were submitted from companies such as Percival and Armstrong Whitworth, Miles' design was selected as the winner, with the company being issued an instruction to proceed with development during October 1944. As per the convention at the time, development and ordering were overseen by the Air Ministry alone, with Miles being forbidden from directly communicating with commercial operators to seek input on their requirements or suggestions.
By April 1945, the majority of the design features for the aircraft, which was designated M.60 Marathon, had been agreed upon. The Marathon incorporated numerous modern features, including its all-metal construction, being the first Miles-built aircraft to be built as such, as well as being the company's first four-engined design. Around this latter stage of development, work was protracted by a multitude of state agencies becoming involved and pushing for their own diverse requirements to be incorporated, some of which were contradictory and occasionally impractical to achieve, such as the use of a pressurised cabin or a very high level of structural strength. This led to numerous disputes over which groups had authority to overrule one another and led to considerable resource waste on the project.
A total of three prototypes were built for the development process, the first of which performed the type's maiden flight on 19 May 1946. Flight testing of the Marathon yielded positive results from the onset; during its official trials, the aircraft was described as being the nicest multi-engined aeroplane to have ever been handled by its test pilots. It was also recognised that the Marathon was the first British transport aircraft to comply with the stringent International Civil Aviation Organization (ICAO) safety requirements. However, on 10 May 1948, tragedy struck when one of the prototypes was lost during official trials held at RAF Boscombe Down; the loss was attributed to pilot error, having failed to adjust the fins to their normal position, resulting in mid-flight structural failure.
While Miles had worked on the Marathon under its instructions to proceed, the issuing of a production contract by British authorities was anything but prompt. The second prototype was in flight and the third was at an advanced stage before negotiations towards such a contract were successful, but by then it was too late for the company. Miles had experienced persistent financial difficulties and was banking on at least 100 Marathons being ordered; however, the initial production contract that emerged only ordered 50 aircraft, of which 30 were intended for British European Airways (BEA) while 20 were directed to British Overseas Airways Corporation (BOAC), which already intended to resell its aircraft onto other airlines.
Recent media