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hesham said:Thanks my dear Jemiba,
Hawker HS.132 was 164 passenger airliner project and HS.134 was
210 passenger airliner project.
Would someone mind explaining the the specific variants of the HS.136 mentioned here? I'm particularly confused as to which ones had engines under their wings and which ones had them at the rear of the fuselage, and the order of events in which they were developed/appearedFrom this book.
Would someone mind explaining the the specific variants of the HS.136 mentioned here? I'm particularly confused as to which ones had engines under their wings and which ones had them at the rear of the fuselage, and the order of events in which they were developed/appeared
Unlike the previous reply, I will try and give you a more detailed answer. The first iteration of the HS.136 had straight wings and a T Tail with rear mounted engines. That was first conceived in May 1964. Engines were RB.172 and passenger capacity was between 36 and 40. July 1966 saw a revision with the capacity raised to 50. A more swept wing was introduced, together with new powerplants in the shape of the RR Trent, although still rear mounted at this time. In January 1967 a new revision saw the underwing engine arrangement, still keeping the Trent. Also the tailplane was moved to the lower position. However, with competing designs also coming from Manchester, the HS board decided that any efforts in this sector would be best served by joint efforts from the two teams. This led on 1968 to the HS.144.Would someone mind explaining the the specific variants of the HS.136 mentioned here? I'm particularly confused as to which ones had engines under their wings and which ones had them at the rear of the fuselage, and the order of events in which they were developed/appeared
Unlike the previous reply, I will try and give you a more detailed answer. The first iteration of the HS.136 had straight wings and a T Tail with rear mounted engines. That was first conceived in May 1964. Engines were RB.172 and passenger capacity was between 36 and 40. July 1966 saw a revision with the capacity raised to 50. A more swept wing was introduced, together with new powerplants in the shape of the RR Trent, although still rear mounted at this time. In January 1967 a new revision saw the underwing engine arrangement, still keeping the Trent. Also the tailplane was moved to the lower position. However, with competing designs also coming from Manchester, the HS board decided that any efforts in this sector would be best served by joint efforts from the two teams. This led on 1968 to the HS.144.