B-1A Generalities Flashcards

0
Q

What is the height of the B-1A?

A

33’ 7”

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1
Q

What is the length of the B-1A?

A

157’ 6”

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2
Q

In the swept position, the sweep back angle is:

A

67.5 degrees.

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3
Q

In the spread position the sweep back angle is:

A

15.0 degrees.

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4
Q

The sweep range of the wings is:

A

52.5 degrees.

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5
Q

The wing area (S) in the spread position is:

A

1,946 sq. ft.

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6
Q

The aspect ratio of the B-1A wings is:

A

AR = 9.0

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7
Q

How many pressurized compartments does the B-1A have?

A

One (the cockpit).

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8
Q

How many sections does the segmented rudder have?

A

Three sections.

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9
Q

The B-1A is powered by four:

A

F101-GE-100 low BPR, augmented turbofans.

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10
Q

What control surfaces are used to generate (L) rolling moments?

A

The horizontal stabilators.

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11
Q

The F101-GE100 turbofan generates (SLS conditions, max augmentation) how much thrust?

A

29,850 lbf.

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12
Q

What grade fuel is used for the B-1A?

A

Wide-cut JP-4.

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13
Q

What type of oil is used?

A

Synthetic oil.

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14
Q

The airplane has a maximum fuel capacity of:

A

39,711 lbs.

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15
Q

The MTOW is:

A

360,000 lbs.

16
Q

The MLW is:

A

346,500 lbs.

17
Q

The OEW is:

A

~143,000 lbs.