Hawker Siddeley Trident
1962
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Hawker Siddeley Trident

Designed by De Havilland later incorporated into Hawker Siddeley Group. First flew on January 9, 1962. 117 built.

3-View 
Hawker Siddeley TridentA three-view drawing (592 x 907)


Specification 
 MODELTrident 2E
 CREW3
 PASSENGERS140
 ENGINE4 x Rolls-Royce Spay RB.163-25 Mk 512-5W turbo-fans, 53.2kN
 WEIGHTS
    Take-off weight65318 kg144002 lb
    Empty weight33203 kg73200 lb
 DIMENSIONS
    Wingspan29.87 m98 ft 0 in
    Length34.98 m115 ft 9 in
    Height8.23 m27 ft 0 in
    Wing area135.26 m21455.93 sq ft
 PERFORMANCE
    Cruise speed974 km/h605 mph
    Ceiling9100 m29850 ft
    Range3965 km2464 miles

Comments 
Barry, 19.06.2009

The Trident 2E had three Rolls Royce Spey RB163-25 Mk512 turbo fans as noted.The original engine was to be the still born R.R.Medway DeHavillands having to replace this with the Spey (essentially a military engine. As correctly noted the Trident 3 had a fourth engine namely a tail mounted R.B.162 booster engine to enable it to get off the ground!

Frank, f.a.cook(@)btinternet.com, 29.05.2009

The engine was the Spey - a Scottish river a few miles from Lossiemouth. NB all RR jets are named after rivers - from Derwent to Trent. If the site owners fix the typo, please remove this comment.

Tom Ensign, 01.07.2008

Does the Hawker Siddeley "Trident" 2E REALLY have four engines? The Trident 3B had four, but one was much smaller than the R-R Spay.

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