SIPA S.1100

Airplanes

Length

11.3 m

Flat Wing Span

14.7 m

Height

3.75 m

Max Speed

380 km/h

Number of Engines

Aircraft Engine

First Flight

1958-04-24

Number Built

Maximum Take-Off Weight

6.2 t (paragliders: kg)

Maximum Range

2000 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
SIPA S.1100	6.2	2000

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Mitsubishi Ki-46		11	14.7	Compare
Bell P-59 Airacomet		11.5824	13.716	Compare
Naval Aircraft Factory TDN	Lycoming O-435	11.2776	14.6304	Compare
Nakajima J5N Tenrai		11.46	14.4	Compare
Fairchild AT-21 Gunner	Ranger V-770	11.5824	15.8496	Compare
Gloster F.9/37		11.2776	15.24	Compare

All data (17 fields)

Name: SIPA S.1100
Manufacturer: Société Industrielle pour l'Aéronautique
Description: The SIPA S.1100 was a French twin engine observation and ground support aircraft flown in 1958.
First Flight: 1958-04-24
Designer: Yves Gardan
Length (m): 11.3
Height (m): 3.75
Cockpit Crew: 3
Max Speed (km/h): 380
Armament: 2×20 mm
National Origin: France
Number Built: 1
Powerplant Description: 2 × Pratt & Whitney R-1340 Wasp 9 cylinder radial, 455 kW (610 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/SIPA_S.1100
Flat Wing Span (m): 14.7
Aircraft Engine: Pratt & Whitney R-1340 Wasp
Number of Engines: 2