Accession Number : ADP005616
Title : Propulsion System Technologies for Thrust Vectoring,
Corporate Author : ROLLS-ROYCE LTD BRISTOL (ENGLAND)
Personal Author(s) : Pound,P. ; Tape,R. F.
Report Date : DEC 1986
Pagination or Media Count : 12
Abstract : The Harrier/AV-8 aircraft, with its Rolls-Royce Pegasus engine, was developed primarily for vertical or short takeoff and landing operations. To achieve this it employs nozzles capable of vectoring through more than 90 deg to provide 'lift' and a reaction control system to provide aircraft have also been employed to achieve a tactical advantage during combat by vectoring in forward flight (VIFFING). Operational analysis studies have identified the potential combat advantage of post-stall manoeuvring (PSM) to improve rate of turn and vehicle/weapon pointing. To achieve any or all of these capabilities (ie V/STOL, VIFF and PSM) will require some degree of propulsion system thrust vectoring. Some particular requirements that the need for thrust vectoring place on the engine design and the technologies involved are addressed in this paper.
Descriptors : *SHORT TAKEOFF AIRCRAFT, *THRUST VECTOR CONTROL SYSTEMS, *ATTACK AIRCRAFT, PROPULSION SYSTEMS, AERODYNAMIC STABILITY, FLIGHT MANEUVERS, AIR INTAKES
Subject Categories : V/STOL
Attack and Fighter Aircraft
Distribution Statement : APPROVED FOR PUBLIC RELEASE