Volume 1
MIL-HlLBK-162A
Section 2
15 December 1965
ITEM NAME: TILT STABILIZATION ASSEMBLY
TYPE: AN/APA-15
RELATION TO SIMILAR EQUIPMENT
Rotary Converter Power Data
Input: 26v de, 10 amps
None.
Output: 115v, 100 cps, 3-ph, 0.502
amp s
TECHNICAL DESCRIPTION
INSTALLATION CONSIDERATIONS
Compensation Limits: plus or minus 30 deg
Accuracy: plus or minus 1 deg Not available.
PRINCIPAL COMPONENTS AND PHYSICAL DATA
COMPONENTS
QTY
OVERALL DIMENSIONS
UNIT WT.
(Inches)
(Pounds)
1
7-3/1 x 8-3/-4 x 15-3/16
13
Servo Amplifier AM-21/APA-15
1
1-19/32 x 6-5/16 x 7-3/16
7
Mounting Base MT-131/APA-15
1
1-7/8 x 6-3/5 x 20-1/4
2
Rotary Converter Pt'U-l11/APA-15
1
5-1/4 x 6-1/16 x 9-1/8
9.5
REFERENCE DATA AND LITERATURE
Technical Manuals:
CO-AN-Ot-30APS15-2 for Model AN/APS-15 Aircraft
Radar Equipment.
Nomenclature Card for Tilt Stabilization
Assembly AN/APA-15.
AN/APA-15: 2