The Super VC10
NOW operating on North Atlantic routes in service with British Overseas Airways Corporation, the Super VC10 is a ‘stretched’ version of the Standard VC10 which B.O.A.C. has been flying for the last twelve months on Middle Eastern, African and Far Eastern routes. Developed to carry higher payloads ov...
Published in: | Aircraft Engineering and Aerospace Technology |
---|---|
Format: | Article in Journal/Newspaper |
Language: | English |
Published: |
Emerald
1965
|
Subjects: | |
Online Access: | http://dx.doi.org/10.1108/eb034003 https://www.emerald.com/insight/content/doi/10.1108/eb034003/full/xml https://www.emerald.com/insight/content/doi/10.1108/eb034003/full/html |
id |
cremerald:10.1108/eb034003 |
---|---|
record_format |
openpolar |
spelling |
cremerald:10.1108/eb034003 2024-06-09T07:48:11+00:00 The Super VC10 1965 http://dx.doi.org/10.1108/eb034003 https://www.emerald.com/insight/content/doi/10.1108/eb034003/full/xml https://www.emerald.com/insight/content/doi/10.1108/eb034003/full/html en eng Emerald https://www.emerald.com/insight/site-policies Aircraft Engineering and Aerospace Technology volume 37, issue 4, page 109-112 ISSN 0002-2667 journal-article 1965 cremerald https://doi.org/10.1108/eb034003 2024-05-15T13:23:58Z NOW operating on North Atlantic routes in service with British Overseas Airways Corporation, the Super VC10 is a ‘stretched’ version of the Standard VC10 which B.O.A.C. has been flying for the last twelve months on Middle Eastern, African and Far Eastern routes. Developed to carry higher payloads over longer ranges than the Standard VC10, the Super VC10 differs principally in having a longer fuselage (a 6 ft. extension having been introduced ahead of the wing and a 7 ft. extension aft of the wing), four Conway R.Co.43 by‐pass turbojets of 22,500 lb. static thrust each in place of the four 21,000 lb. thrust Conway R.Co.42 engines as well as increased fuel capacity in the form of an integral fuel tank in the fin. Further details of the manner in which the two versions differ are provided in this issue of AIRCRAFT ENGINEERING—which is devoted entirely to engineering aspects of Britain's latest long‐range airliner. Article in Journal/Newspaper North Atlantic Emerald Conway ENVELOPE(-61.422,-61.422,-62.841,-62.841) Aircraft Engineering and Aerospace Technology 37 4 109 112 |
institution |
Open Polar |
collection |
Emerald |
op_collection_id |
cremerald |
language |
English |
description |
NOW operating on North Atlantic routes in service with British Overseas Airways Corporation, the Super VC10 is a ‘stretched’ version of the Standard VC10 which B.O.A.C. has been flying for the last twelve months on Middle Eastern, African and Far Eastern routes. Developed to carry higher payloads over longer ranges than the Standard VC10, the Super VC10 differs principally in having a longer fuselage (a 6 ft. extension having been introduced ahead of the wing and a 7 ft. extension aft of the wing), four Conway R.Co.43 by‐pass turbojets of 22,500 lb. static thrust each in place of the four 21,000 lb. thrust Conway R.Co.42 engines as well as increased fuel capacity in the form of an integral fuel tank in the fin. Further details of the manner in which the two versions differ are provided in this issue of AIRCRAFT ENGINEERING—which is devoted entirely to engineering aspects of Britain's latest long‐range airliner. |
format |
Article in Journal/Newspaper |
title |
The Super VC10 |
spellingShingle |
The Super VC10 |
title_short |
The Super VC10 |
title_full |
The Super VC10 |
title_fullStr |
The Super VC10 |
title_full_unstemmed |
The Super VC10 |
title_sort |
super vc10 |
publisher |
Emerald |
publishDate |
1965 |
url |
http://dx.doi.org/10.1108/eb034003 https://www.emerald.com/insight/content/doi/10.1108/eb034003/full/xml https://www.emerald.com/insight/content/doi/10.1108/eb034003/full/html |
long_lat |
ENVELOPE(-61.422,-61.422,-62.841,-62.841) |
geographic |
Conway |
geographic_facet |
Conway |
genre |
North Atlantic |
genre_facet |
North Atlantic |
op_source |
Aircraft Engineering and Aerospace Technology volume 37, issue 4, page 109-112 ISSN 0002-2667 |
op_rights |
https://www.emerald.com/insight/site-policies |
op_doi |
https://doi.org/10.1108/eb034003 |
container_title |
Aircraft Engineering and Aerospace Technology |
container_volume |
37 |
container_issue |
4 |
container_start_page |
109 |
op_container_end_page |
112 |
_version_ |
1801379789925253120 |