| Type | Aircraft | |
| Company | Douglas Aircraft Company | |
| Scheme | Concept High wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
16.2
88.7
|
|
| Height (m) |
0.6
5.5
50.1
|
|
| Wings | ||
| Wingspan (Beam) (m) |
0.1
21.3
95
|
|
| Weights | ||
| Max. takeoff weight (Gross weight) (kg) |
154
27,215.5
575,000
|
|
| Loaded weight (kg) |
5
22,680
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
3
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
879
28,165
|
|
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.4
2.1
|
|
| Thrust (kN) |
1.5
91
1,914
|
2 powerplants 45,5 kN each |
| Performance | ||
| Service ceiling (m) |
0.6
14,000
161,544
|
|
| Combat | ||
| Missiles (qt) |
1
6
24
|
AAM-N-10 Eagle air-to-air missiles |
| Stat | ||
| Number built (qt) |
0
1
43,000
|
|
| Introduction | 1961 | |
