Douglas A-4M - Page 36

Section XI
Part 4
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24
22
20
18
1.
14
12
MODEL: A-4M
ENGINE: J52-P-40&
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NAVAIR Ol-40AVM - l
MAXIMUM RANGE CRUISE
NAUTICAL MILES PER POUND OF FUel
DATA AS OF:
15 OCTOBER 1971
DATA BASIS : ESTIMATED
PRESSURE
ICAO
ALTITUDE STANDARD
- 1000
FT . TEMP . - ·C
I
I
I
I
I
OPTIMUM CRUISE
ALTITUDE AT
DRAG INDEX
o
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.... 200
0
5
10
15
20
25
30
35
40
SPECIFIC RANGE
15.0
5 .1
-4.&
-14 .7
-24 .6
-34 .5
-44.4
-54 .3
-56 .5
- NAUTICAL MILES PER POUND OF FUel
o
u-
75
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t.Ij -so
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.-25·
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.05 .10 .15 .20 .25 . 30 .35
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BASELINE !Z
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BASELINE
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Figure 11- 28. Maximum Range Cru i se - Na utical Mil es per Pound 01 ,l< 'uel