FMA SAIA 90

Airplanes

Length

15.53 m

Flat Wing Span

10.95 m

Height

3.96 m

Flat Wing Area

30 m²

Max Mach

2.25 Mach

Max Ceiling

15000 m

Number of Engines

Aircraft Engine

Number Built

Maximum Take-Off Weight

14.5 t (paragliders: kg)

Maximum Range

3380 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
FMA SAIA 90	14.5	3380

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
British Aerospace EAP	Turbo-Union RB199	14.6304	11.5824	Compare
Yakovlev Yak-25		15.665	10.964	Compare
Convair F2Y Sea Dart		15.5448	10.668	Compare
Northrop YF-17		16.764	10.668	Compare
Fairchild BQ-3	Ranger V-770	15.8496	11.2776	Compare
Gloster Meteor F8 "Prone Pilot"		15.8496	11.2776	Compare

All data (21 fields)

Name: FMA SAIA 90
Manufacturer: Fabrica Argentina de Aviones
Description: The FMA SAIA 90 was a cancelled air superiority fighter aircraft project, designed by the FMA (Fábrica Militar de Aviones) with the collaboration of Dornier in the mid-1980s.
Designer: Fabrica Argentina de Aviones
Type: Air superiority fighter
Length (m): 15.53
Height (m): 3.96
Cockpit Crew: 1
Max Ceiling (m): 15000
Rate of Climb (m/s): 250
Max Mach (Mach): 2.25
National Origin: Argentina
Number Built: 0
Powerplant Description: 2 × GE F404 afterburning turbofan
Primary Users: Argentine Air Force (planned)
Status: Cancelled
Wikipedia Article (URL): en.wikipedia.org/wiki/FMA_SAIA_90
Flat Wing Span (m): 10.95
Flat Wing Area (m²): 30
Aircraft Engine: General Electric F404
Number of Engines: 2