Douglas A-4M - Page 18

68 pages

Save Page as PDF

To Next Page

To Next Page

To Previous Page

To Previous Page

Loading...

Section

XI

Part

2

110

160

~

~

0

Z

ISO

'"

I

Q

140

w

w

~

~

~

•

130

Q

w

~

120

•

U

Q

~

20

-2

0

2

11- 22

HALF

FLAPS

MODEl:

A-4M

ENGINE: JS2-P-408

NAVA

IR

Ol-4

0AVM- l

TAKEOFF

DISTANCE

OPERATIONAL

18

0

NOSEUP TRIM)

NO

JATO

DATA

AS

OF: 1

DECEMBER

1970

DATA

BASIS:

FLIGHT

TEST

INAVY)

~TTrrMn~"~~-rnc~~r"~

rJ

~'~'~'

~

I

1

j:

-

--.,,-

'\

,

\

\

-'-

\,

0 I

._t

..#

~t+

AK:EOFF

AlRSP..Ef

l '

1 • -t r

.

'."

, '

"1<IMOM

rJiJt£6

F

'W

I\1GHT

1.

~

.•

'.

!",AT

IE

LIMITED

BV

, SAfE

.....

L

y';'

. + .

~

f1.E

SPEED

OF

115J<NOT~

;

. .

"'r·;

~

ROUND

SPEED

.

SEE

MAXIMUM

1::-t.:

..

~

~i;

l

AKEdF£

~E1GHT

'

CHA

-:

T :

r

PRESSURE

AtTITUDE

5

6

-

80

,= 100

~-

-

-

120

BASELINE

8 •

7

FEET

FA

1

-14S-A

Figu

r e 11-

8.

Takeof

f

Distance