| Country
of Origin: |
USA |
| Manufacturer: |
Rockwell
International, North American Aircraft |
| Designation: |
B-1 |
| Version: |
B |
| Nickname: |
Lancer |
| Type: |
Long-Range
Strategic Bomber |
| Crew: |
4
- Aircraft Commander, Pilot,
Offensive
System Officer, Densive System Officer |
| First
flight: |
June
1985 |
| Inventory: |
100 |
| Unit
prise: |
$200+
million |
|
|
|
Performance
|
|
| Ceiling: |
normal |
14
600 m / 47 900 ft |
| maximum |
n.a |
| Combat
Radius: |
n.a. |
| Flight
Radius: |
without
refueling |
12
000 km / 7 455 miles |
| with
refueling |
n.a. |
| Take-off
distance: |
n.a. |
| Landing
distance: |
n.a. |
| Landing
speed: |
145-195
kts |
| Designed
g limits: |
n.a. |
|
|
| Weights |
|
| Empty: |
86
183 kg / 190 000 lb |
| Normal
takeoff: |
n.a. |
| Maximum
takeoff: |
214
650 kg / 477 000 lb |
| Max
payload: |
n.a. |
|
|
| Dimensions |
|
| Span: |
at
a 15 degrees |
41.67
m / 136 ft 9 in |
| at
a 67.5 degrees |
23.84
m / 78 ft 3 in |
| Lenght: |
44.81m
/ 147 ft |
| Height: |
10.36
m / 34 ft 10 in |
| Wing
aeria: |
181
sq m / 1 950 sq ft |
|
|
| Speed |
|
| Max
speed: |
at
H=0 m |
965
kmh / 600 mph / mach 0.78 |
| at
altitude |
1
324 kmh / 823 mph / mach 1.25 |
| Cruising
speed: |
956
kmh / 595 mph / mach 0.9 |
|
|
| Propulsion |
|
| Powerplant: |
General
Electric F101- GE - 102 |
| Thrust: |
normal |
n.a. |
| with
afterburner |
135
kN / 13 600 kgf |
| Number
of engines: |
4 |
|
|
|
Weapon
systems
|
|
| Primary: |
nuclear,
conventional and smart bombs |
| Air-to-air: |
none |
| Air-to-ground: |
B-28,
B-43, B-61, Mk 62, Mk 65 Mk 82,
CBU 87, CBU
89,
CBU
97, WCMD, JDAM, GBU-27,
AGM-154 JSOW |
| Other: |
n.a. |
| Fire
points: |
3
internal lounchers, 8 external |
|
