NASA AD-1

· NASA · 2 × Microturbo TRS 18

Airplanes

Length

11.83 m

Flat Wing Span

9.85 m

Height

2.06 m

Flat Wing Area

8.64 m²

Max Speed

321.8688 km/h

Max Ceiling

3657.6 m

Number of Engines

Aircraft Engine

First Flight

1979-12-21

Number Built

Total Fuel Capacity

302.8329

Pictures

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Aircraft	Total Fuel Capacity
NASA AD-1	302.8329

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
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All data (21 fields)

Name: NASA AD-1
Manufacturer: NASA
Description: The NASA AD-1 is both an aircraft and an associated flight test program conducted between 1979 and 1982 at the NASA Dryden Flight Research Center, Edwards California, which successfully demonstrated an aircraft wing that could be pivoted obliquely from zero to 60 degrees during flight.
First Flight: 1979-12-21
Service End: 1982-08-01
Designer: Burt Rutan
Type: Experimental aircraft
Length (m): 11.83
Height (m): 2.06
Cockpit Crew: 1
Max Speed (km/h): 321.8688
Max Ceiling (m): 3657.6
National Origin: United States of America
Number Built: 1
Powerplant Description: 2 × Microturbo TRS 18 turbojets
Primary Users: NASA
Wikipedia Article (URL): en.wikipedia.org/wiki/NASA_AD-1
Flat Wing Span (m): 9.85
Flat Wing Area (m²): 8.64
Aircraft Engine: Microturbo TRS 18
Number of Engines: 2