Principal particulars are: Weight loaded, 2800 lb.; overall length, 25 ft. 9 in.; wing span, 29 ft. 3 in.; climb, 6500 ft. in 18 min.
The bristol coupe and hydro-airplane
Aviation
Aviation ; 7 , n 6
1919
1 Fig.
Article (Journal)
English
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The Bristol "Badminton" Airplane
NTRS | 1926
Engineering Index Backfile | 1923
The "Bristol" coupe: 275 HP, Rolls Royce Falcon
Engineering Index Backfile | 1919
Bristol mooring pontoon for hydro-aeroplane
Engineering Index Backfile | 1920
Considerations affecting hydro-ski airplane design
NTRS | 1953
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