VERIFICATION OF SUIT CONTROLLER PERFORMANCE WITH AND WITHOUT PROTECTOR COVER 4TAQ12
Document Type:
Collection:
Document Number (FOIA) /ESDN (CREST):
CIA-RDP75B00285R000400130013-0
Release Decision:
RIPPUB
Original Classification:
K
Document Page Count:
3
Document Creation Date:
December 12, 2016
Document Release Date:
February 27, 2002
Sequence Number:
13
Case Number:
Publication Date:
December 19, 1966
Content Type:
LETTER
File:
Attachment | Size |
---|---|
![]() | 279.3 KB |
Body:
25X1A To:
Approved FOP Release 2002/06/24: CIA-RDP751300285R000400130013-if?
OSA 48St1-6c,
19 December 1966
Subject: VERIFICATION OF SUIT CONTROLLER PERFORMANCE
WITH AND WITHOUT PROTECTOR COVER 4TAQ12
25X1A Dea
The subject cover was to be added to the suit controller to protect
the 02 hoses from damage during aircraft emergencies.
To insure that no additional vent air flow back pressure resulted
from enclosing the controller within the subject cover, 4TAQ12,
the following tests were successfully concluded:
A. Vent airflow at sea level with and without the cover
installed.
B. Vent airflow at normal cabin altitude with and without
the cover installed.
The results shown by the enclosed data indicates that no increase
in back pressure resulted by enclosing the suit controller within
the cover 4TAQ12.
We are presently making twenty covers from our
and will coordinate withl
installation.
meb
Enclosure
prototype cooling
Or
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