Rockwell-MBB X-31

Airplanes

Length

13.21 m

Flat Wing Span

7.26 m

Height

4.44 m

Flat Wing Area

21.02 m²

Max Speed

1449 km/h

Max Mach

1.28 Mach

Max Ceiling

12200 m

Number of Engines

First Flight

1990-10-11

Number Built

Maximum Take-Off Weight

7.228 t (paragliders: kg)

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))
Rockwell-MBB X-31	7.228

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Dassault Balzac V		13.1	7.3	Compare
Hawker Siddeley P.1127		12.8016	6.7056	Compare
Douglas D-558-2 Skyrocket		12.8016	7.62	Compare
Caudron G.2		12.1	7.25	Compare
SNCASE SE.212 Durandal		12.07	7.44	Compare
List of Mikoyan-Gurevich MiG-21 variants	Tumansky R-11	14.5	7.154	Compare

All data (21 fields)

Name: Rockwell-MBB X-31
Manufacturer: Rockwell International
Description: The Rockwell-Messerschmitt-Bölkow-Blohm X-31 is an experimental jet aircraft designed to test fighter thrust vectoring technology.
First Flight: 1990-10-11
Designer: Rockwell International
Type: Experimental aircraft
Length (m): 13.21
Height (m): 4.44
Cockpit Crew: 1
Max Speed (km/h): 1449
Max Ceiling (m): 12200
Rate of Climb (m/s): 218
Max Mach (Mach): 1.28
National Origin: United States of America
Number Built: 2
Powerplant Description: 1 × General Electric F404-GE-400 turbofan engine, 71 kN thrust each
Primary Users: DARPA, NASA , DLR
Wikipedia Article (URL): en.wikipedia.org/wiki/Rockwell-MBB_X-31
Flat Wing Span (m): 7.26
Flat Wing Area (m²): 21.02
Number of Engines: 1