Technical data | |
---|---|
Year | 1936 |
Function | reconnaissater, light bomber |
Crew | 2 |
Engine | M-85 800hp |
Wing Span | 12.0m |
Wing Area | 24.15m2 |
Length | 10.0m |
Empty Weight | 1,940kg |
Maximum Weight | 2,730kg |
Ground level Speed | 366km/h |
High altitude Speed | 447km/h |
Climb to 5,000m | 8.7min |
Range | 840km |
Ceiling | 9000m |
Armament | |
Guns | 2g20mm
3mg7.62mm |
Bombs | 400kg |
![]() |
Development of already tested in 1935 TsKB-27/SR. Unreliable retraction mechanism of the last one and rush to come up with new design killed the progressive project - R-9 had fixed landing gear, providing huge drag. Flight stability also suffered.
Pre-series batch production started, but was aborted in a short time. R-9 lost a contest with Neman's R-10.
Modified June 24, 1997 | ![]() |
Back to Main Gate |