| dc.creator |
Howe, D. |
|
| dc.date |
2016-01-12T14:46:17Z |
|
| dc.date |
2016-01-12T14:46:17Z |
|
| dc.date |
1975-08 |
|
| dc.date.accessioned |
2022-05-09T10:22:49Z |
|
| dc.date.available |
2022-05-09T10:22:49Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/9638 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4855 |
|
| dc.description |
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. |
|
| dc.language |
en |
|
| dc.publisher |
Cranfield Institute of Technology, College of Aeronautics |
|
| dc.relation |
CIT/CoA/Aero-31 |
|
| dc.relation |
31 |
|
| dc.title |
Aircraft design studies: S68 multi-role strike aircraft |
|
| dc.type |
Report |
|