| Type | Aircraft | |
| Company | Douglas Aircraft Company | |
| Scheme | Midwing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
12.8
88.7
|
|
| Height (m) |
0.6
3.8
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
16.3
925
|
|
| Wingspan (Beam) (m) |
0.1
7.6
95
|
|
| Wing loading (kg/m2) |
3.1
426
829
|
|
| Weights | ||
| Empty weight (kg) |
8
4,273.3
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
6,924.5
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
1,160
28,165
|
|
|
25
2,010
28,165
|
when air-launched | |
| Stall Speed (km/h) |
40
257.7
257.7
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
950
320,000
|
of aviation fuel |
| Power | ||
| Thrust/weight (kN/kg) |
0.0
0.4
2.1
|
jet |
| Thrust (kN) |
1.5
40
1,914
|
2 powerplants 13 kN one and 27 kN another |
| Performance | ||
| Service ceiling (m) |
0.6
5,029.2
161,544
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
6,827.5
36,000
|
|
|
1.9
3,380
36,000
|
under rocket power only | |
| Stat | ||
| Number built (qt) |
0
3
43,000
|
|
| Introduction | 1948 | |
| First flight | 04.02.1948 | |
