Aircraft design studies: S68 multi-role strike aircraft

Show simple item record Howe, D. 2016-01-12T14:46:17Z 2016-01-12T14:46:17Z 1975-08
dc.description.abstract The 868 aircraft design study was for a multi-role strike aircraft with a variable sweepback wing. The study was undertaken as the result of experience gained in a previous investigation of a naval strike aircraft, the 864 (Ref.1). The more recent design was for a land based aircraft intended to be capable of fulfilling strike, interception and search roles. The design take off weight was 50,000 lbs and the normal maximum speed condition was Mach 2 at altitude although a short dash to M 2.5 was catered for. An internal bay was provided for the carriage of various combinations of stores. Side by side seating was adopted for the two crew members and some difficulty was experienced with the structural layout of the fuselage and the design of the main undercarriage because of this. en_UK
dc.language.iso en en_UK
dc.publisher Cranfield Institute of Technology, College of Aeronautics en_UK
dc.relation.ispartofseries CIT/CoA/Aero-31 en_UK
dc.relation.ispartofseries 31 en_UK
dc.title Aircraft design studies: S68 multi-role strike aircraft en_UK
dc.type Report en_UK

Files in this item

This item appears in the following Collection(s)

Show simple item record

Search CERES


My Account