DESIGN OF AN ACCELERATION TRANSMITTER FOR USE WITH GUIDED MISSILES' STEERING MECHANISMS

• Document Type: CREST
• Collection: General CIA Records
• Document Number (FOIA) /ESDN (CREST): CIA-RDP80-00810A001300070008-1
• Release Decision: RIPPUB
• Original Classification: S
• Document Page Count: 5
• Document Creation Date: December 19, 2016
• Sequence Number: 8
• Content Type: REPORT

Approved For Release 2006/11/20: CIA-RDP80-0081OA001300070008-1
CENTRAL INTELLIGENCE AGENCY
INFORMATION REPORT
SECRET
SECURITY INFORMATION
COUNTRY USSR (Kalinin Oblast)
SUBJECT
25X1 DATE OF INFO.
PLACE ACQUIRED
THE SOURCE EVALUATIONS IN THIS REPORT ARE DEFINITIVE.
THE APPRAISAL OF CONTENT IS TENTATIVE.
(FOR KEY SEE REVERSE)
25X1
further information on e m ss e, and my assumptionha the m ss e
was to be ground-controlled is based only on the design peculiarities
of the accelerometer fdescribed in this reporg.
Two accelerometers installed at right angles to each other in the misi.1-.
comprised a single unit.'.A space was left in the mounting case for ac..-
ditional electrical equipment, of what type I do not know.
The technical requirements for the acceleration transmitters were pri.
marily the following:
a. Plus-minus 8 Gs static and low frequency acceleration..
b.. Unit to function in only one acceleration direction.
c. Maximum unilateral and torsion acceleration error to be less
than 0.5 percent.
d. Power output at the exit poles of the bridge to be 5 ma. at
2,000 ohms.
SOURCE:
fix-
ARMY .#x INAVY #x IAIR
W
This Document contains Information affecting? the Ha
tidnal Defense of the United States, within the mean-
Ing of Title 18, Sections 793 and 794, of the U.S. Oode, as
amended. Its transmission or revelation of its contents
to or receipt by an unauthorized person Is prohiblted
by law. The reproduction of this form is prohibited.
Design of an Acceleration Transmitter DATE DISTR.
for Use with Guided Missiles' Steer-
ing Mechanisms C. OF PAGES
28 MEq 1953
25X1
Approved For Release 2006/11/20: CIA-RDP80-0081OA001300070008-1
 Approved For Release 2006/11/20: CIA-RDP80-0081OA001300070008-1
SECRET'
Highest possible linear reliance on the measuring
value of acceleration: permissible deviation plug:''..
minus 5% of the maximum scale value.
The absolute error of the measurement value itself
was to be less than 1% of the maximum scale value.
g. Temperature range fzo m plus 400 50 degr ej
air presR Y , ` r a T , o . & : to u, 3 r~n~ aa? x
Insulation resistance minimum 50 M Ohm under 10O
moisture conditions.,
i. Insulating value (dielect:.1.-- lltrength) of the coils
toward each Other: mii, mu=.r:. 5iC lts; and .:.gat ?e
mass , minimum 250 volts.
The acceleration transmitter was built in two parts which
were virtually identical and had one connection plug for
the entire unit. glee c.tc]'a? s or :age. A spring
suspended sass v