Scaled Composites Triumph

Airplanes

Length

11.8872 m

Flat Wing Span

14.6304 m

Height

3.32 m

Flat Wing Area

18.4877 m²

Flat Wing Aspect Ratio

11.55

Cruise Speed

629.6795 km/h

Max Speed

740.2982 km/h

Max Ceiling

12496.8 m

Number of Engines

Aircraft Engine

First Flight

1988-07-12

Number Built

Maximum Take-Off Weight

4.0823 t (paragliders: kg)

Maximum Range

2963.2 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Scaled Composites Triumph	4.0823	2963.2

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Reims-Cessna F406 Caravan II		11.89	15.09	12	Compare
Cessna 404 Titan		11.8872	14.0208	8	Compare
Rockwell 685	Continental IO-520	12.8016	14.0208	8	Compare
Dornier Do 28	Lycoming O-540	11.41	15.55	12	Compare
Piaggio P.166		11.88	13.51	8	Compare
Lockheed Model 12 Electra Junior		10.9728	14.9352	6	Compare

All data (22 fields)

Name: Scaled Composites Triumph
Manufacturer: Scaled Composites
Description: The Scaled Composites Triumph is a twin-engine, business jet prototype designed and built by Burt Rutan's Scaled Composites for Beechcraft.
First Flight: 1988-07-12
Designer: Burt Rutan
Type: Very Light Jet demonstrator
Length (m): 11.8872
Height (m): 3.32
Max Speed (km/h): 740.2982
Cruise Speed (km/h): 629.6795
Min Speed (km/h): 138.8999
Max Ceiling (m): 12496.8
Rate of Climb (m/s): 22.86
National Origin: United States of America
Number Built: 1
Powerplant Description: 2 × Williams FJ44 turbofans
Wikipedia Article (URL): en.wikipedia.org/wiki/Scaled_Composites_Triumph
Flat Wing Span (m): 14.6304
Flat Wing Area (m²): 18.4877
Flat Wing Aspect Ratio: 11.55
Aircraft Engine: Williams FJ44
Number of Engines: 2