McDonnell Douglas A-12 Avenger II

Length
11.2776 m
Flat Wing Span
21.336 m
Height
3.3528 m
Flat Wing Area
121.5172 m²
Max Speed
925.9992 km/h
Max Ceiling
12192 m
Number of Engines
2
Number Built
0
Maximum Take-Off Weight
36.2874 t (paragliders: kg)

Pictures

No pictures yet for this family.

Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg))
McDonnell Douglas A-12 Avenger II 36.2874

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
Tupolev ANT-21 Mikulin AM-34 11.57 20.76 Compare
Caudron R.4 11.8 21.1 Compare
Siebel Si 204 11.95 21.33 8 Compare
Friedrichshafen G.I Benz Bz.III 11.9 21.2 Compare
Hansa-Brandenburg GW Mercedes D.III 11.9 21.56 Compare
Borel-Odier Bo-T 11.23 20 Compare
All data (20 fields)
Name
McDonnell Douglas A-12 Avenger II
Manufacturer
General Dynamics
Description
The General Dynamics/McDonnell Douglas A-12 Avenger II was a proposed American attack aircraft from General Dynamics and McDonnell Douglas.
Designer
General Dynamics
Type
All-weather naval stealth bomber
Length (m)
11.2776
Height (m)
3.3528
Cockpit Crew
2
Max Speed (km/h)
925.9992
Max Ceiling (m)
12192
Rate of Climb (m/s)
25.4
Armament
Payload capability: 5160 lb in internal weapons bay including: :* 2× AIM-120 AMRAAM air-to-air missiles :* 2× AGM-88 HARM air-to-ground missiles :* Unguided or precision-guided bombs
Number Built
0
Powerplant Description
2 × General Electric F412-GE-D5F2 turbofan engines, 58 kN thrust each
Primary Users
United States Navy, United States Marine Corps
Status
Canceled
Wikipedia Article (URL)
en.wikipedia.org/wiki/McDonnell_Douglas_A-12_Avenger_II
Flat Wing Span (m)
21.336
Flat Wing Area (m²)
121.5172
Number of Engines
2