Altitude (ft)

S.L.

20,000

40,000

Mach

0.25

0.7

0.7

True Airspeed (ft/s)

279

725

678

Dyn Pressure (lb/ft ²)

Weight (lb)

728,000

728,000

728,000

Wing Area S (ft ²)

6,200

6,200

6,200

Wing Span b (ft)

219.17

219.17

219.17

Wing Chord c (ft)

30.93

30.93

30.93

C.G. (x c)

0.25

0.25

0.25

Trim AOA (deg)

11.41

0.68

7.66

I _{xx S}(slug-ft ²)

3.25 10 ⁷

3.23 10 ⁷

3.22 10 ⁷

I _{yy S} (slug ft ²)

3.28 10 ⁷

3.28 10 ⁷

3.28 10 ⁷

I _{zz S} (slug ft ²)

6.15 10 ⁷

6.18 10 ⁷

6.19 10 ⁷

I _{xz S} (slug ft ²)

?3.34 10 ⁶

2.2 10 ⁶

?1.42 10 ⁶

Longitudinal Derivatives

X _u (1/s)

?0.0111

?0.00283

?0.00339

X _? (ft/s ²)

?5.58

19.1

8.43

Z _u (1/s)

?0.107

?0.042

?0.06

Z _? (ft/s ²)

?124

?450

?204

M _u (1/ft s)

?0.00007

?0.00004

0.00005

M _? (1/s ²)

?0.76

?2.2

?1.07

(1/s)

?0.169

?0.21

?0.113

M _q (1/s)

?0.67

?0.898

?0.426

X _{? e} (ft/s ²)

0

0

0

Z _{? e} (ft/s ²)

?11.5

?27.7