Speedtwin E2E Comet 1

Airplanes

Length

6.96 m

Flat Wing Span

7.92 m

Height

2.08 m

Flat Wing Area

11.4 m²

Max Speed

386 km/h

Number of Engines

Aircraft Engine

First Flight

1991-09-30

Number Built

Maximum Take-Off Weight

1.111 t (paragliders: kg)

Total Fuel Capacity

400

Maximum Range

1666 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Speedtwin E2E Comet 1	1.111	400	1666

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Microjet 200		6.67	7.56	Compare
Carden-Baynes Bee	Carden-Ford	7.0104	8.8392	Compare
Bugatti Model 100		7.62	8.2296	Compare
Johnson Twin-60		6.4008	8.5344	Compare
Messerschmitt Me 328	Argus As 014	7.17	6.9	Compare
Scaled Composites Pond Racer		6.096	7.62	Compare

All data (19 fields)

Name: Speedtwin E2E Comet 1
Manufacturer: Peter J. C. Phillips
Description: The Speedtwin E2E Comet 1, originally named the Phillips ST1 Speedtwin, is a two-seat, twin engined aircraft designed in the UK to be capable of aerobatics and the only civil twin certified for intentional spinning.
First Flight: 1991-09-30
Designer: Peter John Croft Phillips
Length (m): 6.96
Height (m): 2.08
Max Speed (km/h): 386
Min Speed (km/h): 120
Rate of Climb (m/s): 10.2
Capacity Description: Two
National Origin: United Kingdom
Number Built: 2
Powerplant Description: 2 × Titan/Lycoming IO-390 flat four, 153 kW (205 hp) each
Wikipedia Article (URL): en.wikipedia.org/wiki/Speedtwin_E2E_Comet_1
Flat Wing Span (m): 7.92
Flat Wing Area (m²): 11.4
Aircraft Engine: Lycoming IO-390
Number of Engines: 2