| Country
of Origin: |
USA |
| Manufacturer: |
Rockwell
International, North American Aircraft |
| Designation: |
B-1 |
| Version: |
A |
| Nickname: |
Lancer |
| Type: |
Long-Range
Strategic Bomber Prototype |
| Crew: |
4
- Aircraft Commander, Pilot,
Offensive
System Officer, Densive System Officer |
| First
flight: |
23
December 1974 |
| Inventory: |
4
build (2 crashed and 2 on display) |
| Unit
prise: |
n.a. |
|
|
|
Performance
|
|
| Ceiling: |
normal |
9
144 m / 30 000 ft |
| maximum |
18
900 m / 62 000 ft |
| Combat
Radius: |
n.a. |
| Flight
Radius: |
without
refueling |
9
817 km / 6 100 miles |
| with
refueling |
n.a. |
| Take-off
distance: |
n.a. |
| Landing
distance: |
n.a. |
| Landing
speed: |
n.a. |
| Designed
g limits: |
n.a. |
|
|
| Weights |
|
| Empty: |
n.a. |
| Normal
takeoff: |
176
810 kg / 389 800 lb |
| Maximum
takeoff: |
179
169 kg / 395 000 lb |
| Max
payload: |
52
163 kg / 115 000 lb |
|
|
| Dimensions |
|
| Span: |
extended
forward |
41.67
m / 136.7ft |
| swept
aft |
23.84
m / 78.2ft |
| Lenght: |
45.78
m / 150.2ft |
| Height: |
10.24
m / 33.6ft |
| Wing
aeria: |
n.a. |
|
|
| Speed |
|
| Max
speed: |
at
H=0 m |
1
470 kmh / 914 mph / mach 1.2 |
| at
altitude |
2
333 kmh / 1 450 mph / mach 2.3 |
| Cruising
speed: |
780 kmh / 485 mph / mach 0.7 |
|
|
| Propulsion |
|
| Powerplant: |
General
Electric F101- GE - 100 |
| Thrust: |
normal |
n.a. |
| with
afterburner |
135
kN / 13 600 kgf |
| Number
of engines: |
4 |
|
|
|
Weapon
systems
|
|
| Primary: |
Nuclear
or Conventional bombs |
| Air-to-air: |
none |
| Air-to-ground: |
Nuclear
or Conventional bombs |
| Other: |
n.a. |
| Fire
points: |
3
internal lounchers, 8 external |
