Handley Page H.P.115
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Handley Page H.P.115

Test aircraft designed to test the behaviour of the delta wing at low speeds. The first flight was on August 17, 1961.

Handley Page H.P.115


Specification 
 MODELH.P.115
 CREW1
 ENGINE1 x Bristol Siddeley "Viper 9" turbojet, 860kg
 WEIGHTS
    Take-off weight2290 kg5049 lb
 DIMENSIONS
    Wingspan6.1 m20 ft 0 in
    Length13.7 m44 ft 11 in
    Wing area40.0 m2430.56 sq ft
 PERFORMANCE
    Max. speed400 km/h249 mph
    Range500 km311 miles

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