Ralph Hooper
Ralph Hooper | |
---|---|
Born | Hornchurch, Essex, England | 30 January 1926
Died | 12 December 2022 | (aged 96)
Nationality | British |
Engineering career | |
Discipline | Aeronautics |
Institutions | RAeS |
Employer(s) | Hawker Siddeley |
Significant design | Hawker Siddeley Harrier |
Significant advance | Hawker Siddeley P.1127 |
Awards | Mullard Award (1983, with John Fozard) |
Ralph Spenser Hooper, OBE, FREng, FRAeS (30 January 1926 – 12 December 2022) was an English aeronautical engineer, recognised mostly for his work on the Hawker Siddeley Harrier, specifically in relation to the marriage between the Pegasus engine and the layout of the aircraft, allowing it to safely hover with margins of stability.
Early life
Hooper was born in Hornchurch, then in Essex. He was the son of Marjorie Spenser and Herbert Hooper. He is a distant relative of the poet Edmund Spenser. He went to Hymers College in Hull. Due to the Hull Blitz he was evacuated to Pocklington Grammar School for one and a half terms. His sister was Sheila Spenser Hooper. He became an apprentice at Blackburn Aircraft Company when aged 15 in January 1942, then went to University College Hull (became the University of Hull in 1954), gaining a Diploma in Aeronautics. He was one of the first students to join the Cranfield College of Aeronautics in 1946 and graduated with a Diploma in Aircraft Design in 1948. He joined Hawker Aircraft in 1948.
Career
Hooper was sometimes referred to, with Sir
Hooper was succeeded as Chief Designer of the Harrier in 1965 by (later Professor) John Fozard, who continued in this post until 1978. Fozard became Chief Designer of the supersonic VTOL P1154[3] from October 1963.
Hooper later became Deputy Technical Director of British Aerospace at Kingston upon Thames (the base of Hawker) in Surrey. In 2019 he was awarded the Distinguished Alumnus Award by Cranfield University.[4]
Harrier
Working from 1957 with the designer of the
The first design had an engine that only vectored the thrust from the engine's fan (cool air) - this was only 50% of the engine's total thrust. Vectoring from the high-temperature engine exhaust was not originally contemplated, or thought possible. However he realised that the hot exhaust gases could be bifurcated, as demonstrated on the earlier Hawker Sea Hawk,[5] to provide enough thrust for vertical take off, the fundamental layout of the Harrier.
By March 1958 he had finally arrived at (what would become) the design of the Harrier, with its distinctive

In early 1960, work at NASA's Ames Research Center had demonstrated that transition from vertical to conventional flight would be possible. On 22 June 1960, the project finally received a contract and finance from the Ministry of Aviation. XP831 (now at the Royal Air Force Museum London) first flew (tethered) on 21 October 1960 with a Pegasus 2 engine at Hawker's Dunsfold Aerodrome flown by Bill Bedford. Untethered flight first took place on 19 November 1960. The first conventional flight took place on 13 March 1961 from RAE Bedford, and it was there on 12 September 1961 that the first full transition from vertical to conventional flight took place, surprisingly with little incident. The first crash took place (XP836) on 14 December 1961 with the pilot successfully ejecting. Anhedral tailplanes were introduced in 1962.

In 1964, the prototypes were improved with a more swept wing and a more powerful Pegasus 5 engine, and in November 1964 it was designated as the Hawker Siddeley Kestrel, and was trialled by pilots from the RAF, the German Luftwaffe and the US Air Force at RAF West Raynham until November 1965. It was funded by these other two air forces as well. Hawker had become Hawker Siddeley in 1963.[6]
The Kestrel was only meant to be a development aircraft for the later P.1154, but was what became the Harrier. The RAF was not pleased about this change of events. The Kestrel was developed under Air Staff Requirement 384. The resulting aircraft had a Pegasus 6 engine, with a new design of air intakes, and redesigned wings to improve longitudinal stability. In December 1966, 60 aircraft were ordered by the Government, and by 1967 had been christened as the Harrier.
P.1154
In 1962 he won the NATO

Hawker Siddeley Hawk
Hooper also led the design team for the
Personal life and death
Hooper became a Fellow of the Royal Academy of Engineering in 1999.
Hooper later lived in Ham, London. He died on 12 December 2022, at the age of 96.[7][8]

See also
- John Dale (engineer), Chief Engineer of the Pegasus engine
References
- ^ a b Flight International 22 November 1986 page 61
- ^ Supplement to the London Gazette 3 June 1978 page 6238
- ^ Note: The P.1154 was originally to have been named the "Harrier" but with the cancellation of that aircraft the name was applied instead to a transonic derivative of the Kestrel.
- ^ "Distinguished Alumnus Award for trailblazing Cranfield student".
- ^ Note: The range requirement for the Hawk/Sea Hawk required the rear fuselage to be available for a fuselage fuel tank, making a conventional single rear jet pipe impossible. In the Hawk/Sea Hawk the jet pipe was divided into two which exhausted behind the aircraft's wing roots on either side of the fuselage. The bifurcated exhaust ducts where known within Hawker as "Elephant's trousers".
- ^ Harrier milestones
- ^ "It is with sadness that the Hawker Association Committee has given us the news that Ralph Hooper died peacefully on Monday 12th December 2022, two months short of his 97th birthday". The Aviation Historian on Twitter. 20 December 2022. Retrieved 21 December 2022.
- ^ "Ralph Hooper obituary". The Times. 24 January 2023. Retrieved 24 January 2023.
External links
- Recorded interview Part 1 of 11
- Full transcript of interview in Oral History of British Science for the British Library
- Kingston Aviation
- Interview for Cranfield University
- Ralph Hooper giving a guided tour of a Harrier
- Ralph Hooper describing history of P1127