Length
5.7912 m
Flat Wing Span
6.7056 m
Height
1.8288 m
Flat Wing Area
13.7496 m²
Max Speed
428.0855 km/h
Max Ceiling
9692.64 m
Number of Engines
1
First Flight
1923-09-09
Number Built
3
Maximum Range
278.4165 km

Pictures

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Aircraft Weight Variants

Aircraft Maximum Range (km)
Curtiss R2C 278.4165

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All data (18 fields)
Name
Curtiss R2C
Manufacturer
Military designations USAAS/USAAF/USAF
Description
The Curtiss R2C was a racing aircraft designed for the United States Navy in 1923 by Curtiss.
First Flight
1923-09-09
Designer
Military designations USAAS/USAAF/USAF
Type
Racing aircraft
Length (m)
5.7912
Height (m)
1.8288
Cockpit Crew
1
Max Speed (km/h)
428.0855
Max Ceiling (m)
9692.64
Number Built
3
Powerplant Description
1 × Curtiss D-12A V-12 water-cooled piston engine, 378 kW (507 hp) each
Primary Users
United States Navy, United States Army
Wikipedia Article (URL)
en.wikipedia.org/wiki/Curtiss_R2C
Flat Wing Span (m)
6.7056
Flat Wing Area (m²)
13.7496
Number of Engines
1