MIL-PRF-1/507H
NOTES: - Continued
14
Anode cooling-fin inlet duct for supplying air to the tube cooling system must to insure delivery of air to the entire cross-section of
the inlet, with minimum side leakage.
15
Anode must be grounded effectively, such as through the mounting holes.
16
W aveguide choke coupling flange, modified UG-541/U.
17
All joints of waveguide output assembly to be hermetically tight. "O"-ring silicone-rubber gasket, in accordance with MIL-DTL-
3922/59 shall be used for test.
18
Four #6-32 screws required to attach waveguide choke to tube.
19
High-voltage terminals: Center terminal = heater, outer terminal = heater-cathode.
20
Mounting holes: Entire support and fastening of tube to be effective therein.
21
Point at which temperature shall be measured on cathode bushing.
Referenced documents. In addition to MIL-PRF-1, this document references the following:
MIL-DTL-75
MIL-STD-1311
MIL-DTL-3922/59
Changes from previous issue: The margins of this specification sheet are marked with vertical lines to indicate where changes were
made from previous issue. Deleted table column locations are denoted using asterisks. This was done as a convenience only and the
Government assumes no liability whatsoever for any inaccuracies in these notations. Bidders and contractors are cautioned to evaluate
the requirements of this document based on the entire content irrespective of the marginal or the asterisk notations.
Custodian:
Preparing activity:
Army - CR
DLA - CC
DLA - CC
(Project 5960-3703)
NOTE: The activities listed above were interested in this document as of the date of this document. Since organizations and
responsibilities can change, you should verify the currency of the information above using the ASSIST Online data base at
www.dodssp.daps.mil.
12
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