Figure 2.1 Air-sampling rocket.

Intake Orifice
Filter
N

=

“<4

=----

——-

7
~

<

N

=

-

4

tt

>

Figure 2.2 Diffuser section of air-sampling rocket.

40

;

"7-7
_

1

1

ee

TTT ts eee ose
36"
~|

250" RADIUS

——

—_

|

{

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aor TTT

Select target paragraph3