Bartel BM 5

· Ryszard Bartel · 1 × SPA 6A

Airplanes

Length

7.81 m

Flat Wing Span

11.2 m

Height

3.18 m

Flat Wing Area

31 m²

Flat Wing Aspect Ratio

Cruise Speed

150 km/h

Max Speed

164 km/h

Max Ceiling

3250 m

Number of Engines

Aircraft Engine

First Flight

1928-07-27

Entry Into service

1930-01-01

Number Built

Total Fuel Capacity

260

Maximum Range

450 km

Pictures

No pictures yet for this family.

Aircraft	Total Fuel Capacity	Maximum Range (km)
Bartel BM 5	260	450

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Aero A.200	Walter Bora	7.8	11.1	2	Compare
ANF Les Mureaux 180	Hispano-Suiza 12X	7.83	11.38		Compare
Albatros B.III	Mercedes D.II	7.8	11		Compare
Aurore MB 04 Souris Bulle		7.9248	11.25		Compare
Aeroprakt A-24 Viking		7.78	11	2	Compare
BFW M.29		7.75	11		Compare

All data (26 fields)

Name: Bartel BM 5
Manufacturer: Ryszard Bartel
Description: The Bartel BM 5, initially known as M.5 was a Polish biplane advanced trainer used from 1930 to 1939 by the Polish Air Force, manufactured in the Samolot factory in Poznań.
First Flight: 1928-07-27
Entry Into service: 1930-01-01
Production End: 1930-01-01
Service End: 1939-01-01
Designer: Ryszard Bartel
Type: Trainer aircraft
Length (m): 7.81
Height (m): 3.18
Cockpit Crew: 2
Max Speed (km/h): 164
Cruise Speed (km/h): 150
Min Speed (km/h): 70
Max Ceiling (m): 3250
Rate of Climb (m/s): 4
Number Built: 62
Powerplant Description: 1 × SPA 6A 6-cyl. water-cooled in-line piston engine, 164 kW (220 hp) each
Primary Users: Polish Air Force
Wikipedia Article (URL): en.wikipedia.org/wiki/Bartel_BM_5
Flat Wing Span (m): 11.2
Flat Wing Area (m²): 31
Flat Wing Aspect Ratio: 7
Aircraft Engine: SPA 6A
Number of Engines: 1