1118-01 - Radome Sets - Drawing_93520-E.pdf

REVINSPECTIONLOCATIONCCs

SUMMATION OF CCs

CRITICAL MAJOR MINOR

CLASSIFICATION OF CHARACTERISTICS (CCs)

CLASSIFICATION OF CHARACTERISTICS (CCs)

DISTRIBUTION STATEMENT D. DISTRIBUTION AUTHORIZED TO DEPARTMENT OF DEFENSE

AND THEIR CONTRACTORS: ADMINISTRATIVE/OPERATIONAL USE: 06 AUGUST 2008

OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO NSWCDD,

ANTENNA PRODUCTION AND TESTING FACILITY, BLDG 1530.

27.50

GG

NO FSS IN EBD COVERS

4 ON INSIDE

OF RADOME

R 12.75

INTERSECT

R 16.91 TO

R 20.40 TO

INTERSECT

10X 17.50°

.13

11X .250 MATCH DRILLED

TO TEMPLATE

R 13.13

40°

A

A

C

C

B

B

SHEET 2

ZONE A4

SHEET 2,

ZONE C7

R 17.50

R 13.85

R 17.13

2X .48

8X 18°

F

13 REQD

AR

19.25

.125

.110

4.38

4.16 3.41

(.57)

7.64

E

SECTION A-A

7 10 11

INTERSECT

POINT

SHEET 2,

ZONE C3

R 13.85

2X .07-.10

DETAIL F

SCALE 2 : 1

VIEW ROTATED 40 FOR CLARITY

SCALE: 1/4

SHEET 2,

ZONE A7

FIND

NO.

QTY

REQD

CAGE

CODE PART NUMBER NOMENCLATURE OR DESCRIPTION MATERIAL

OR NOTE

PARTS LIST

14 AR 1UW17 MMMA132T1C3 PWA457

199-05-002 HYSOL EA 934NA A/B KIT

13 AR 52125 5413 TAPE, KAPTON

12 AR 04621 SAE AMS-C-9084, 181 CLOTH, GLASS, CL 2, TY VIII

11 AR 84063 VERSAMID 140 HARDENER

10 AR 54527 MIL-R-9300

SHELL 828 RESIN

9 AR A-A-56032

M43553-I BLK INK, MARKING, EPOXY BASE

8 10 -102 INSERT MOUNTING BLOCK NOTE 8

7 1 -101 SUPPORT RING NOTE 7

6 AR L210100HH/HHC88,

IPC-4101/21 COPPER CLAD GLASS LAMINATE NOTE 2

5 AR 39212 PN2-3/16-OX-3.0

PLASCORE, INC NOMEX HONEYCOMB, .25 THK NOTE 10

4 AR 02SW6 458IAQIII/EX-1522

BRYTE TECHNOLOGIES ASTROQUARTZ III MODIFIED EPOXY PREPREG

3 AR 02SW6 BT250E-IU

BRYTE TECHNOLOGIES EPOXY FILM ADHESIVE

2 AR 02SW6 SAE AMS-C-9084/778IFg

MIL-R-9300/BT250E-1

FIBERGLASS EPOXY PREPREG, CLOTH

FIBERGLASS EPOXY PREPREG, RESIN

1 23 76017 KNBL 1032J

REXNORD INSERT, BLIND THREADED, LOCKING

REVISIONS

REV DESCRIPTION DATE APPROVED

A REDRAWN WITH CHANGE. OLD DESIGN 55910-

0131537-R-B.

B SEE NOR93520-B. 10/01/22 STR

C SEE NOR93520-C. 10/05/22 STR

D SEE NOR93520-D. 12014/11/17 STR

E DIMENSION AND NOTE CHANGES. 2018/07/05

E E E REV REV

STATUS3 2 1 SH

3/16

93520

INTERPRET DRAWING IAW ASME Y14.100

.03 .010 --

C. BRUBECK 09-03-23

DWG NO.

93520

G64

SH REV1 E

CAD MAINTAINED. CHANGES

SHALL BE INCORPORATED BY

THE DESIGN ACTIVITY.

8 7 6 5 4 3 1

D

C

B

A

D

C

B

A

8 7 6 5 4 3 2 1

E-07609NEXT ASSY USED ON

APPLICATION DO NOT SCALE THIS DRAWING

MATERIAL:

REMOVE BURRS AND BREAK SHARP

EDGES .03 MAX

INSIDE CORNERS R .03 MAX.

SURFACE ROUGHNESS 125

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

GENERAL TOLERANCES

ANGLESXXX DECIMALSXX DECIMALS

ENGR

CHECKED

DRAWN

APPROVED FOR DATE

SIZE CAGE CODE

D

GIN DWG NO. REV

SCALE: WEIGHT: SHEET

DEPARTMENT OF THE NAVY

RADOME, FSS

NAVAL SURFACE WARFARE CENTER

DAHLGREN DIVISION

17320 DAHLGREN RD

DAHLGREN, VA 22448-5000

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ENGR

NOTES:

1. MATERIALS USED IN THIS PART SHALL WITHSTAND A CURE

TEMPERATURE OF 250 F AND A CONTINOUS SERVICE

TEMPERATURE OF 200 F.

2. PLACE FSS MATERIAL (FIND NO. 6, ETCHED TO PATTERN IN VIEW D) SO THAT

POLARIZATION FACES INSIDE AND HORIZONTAL POLARIZATION FACES OUTSIDE.

ORIENTATION IN TOP AND BOTTOM OF RADOME IS NOT IMPORTANT. USE TAPE,

FIND NO. 15, TO SPLICE FSS LAMINATE. PLACE EPOXY FILM ADHESIVE, FIND NO. 3 ON BOTH

SIDES OF FSS TO BOND TO HONEYCOMB FIND NO. 5.

3. PAINTING:

A. FIRST COAT: PAINT, EPOXY-POLYAMIDE, GREEN PRIMER, FORMULA 150, TYPE

III IN ACCORDANCE WITH MIL-DTL-24441 AND MIL-DTL-24441/20B

(0.003" TO 0.004" DRY FILM THICKNESS).

B. INSPECT PART/ASSEMBLY FOR VOIDS. IF PRESENT USE COMPATIBLE EPOXY RESIN

MIXED WITH 410 MICROLIGHT FAIRING FILLER IN ACCORDANCE WITH

MANUFACTURERS (WEST SYSTEM, CAGE CODE 7S147) INSTRUCTIONS

TO FILL THE VOIDS. ALLOW TO DRY IN ACCORDANCE WITH MANUFACTURERS

INSTRUCTIONS AND SAND TO A UNIFORM FINISH.

C. SECOND COAT: PAINT, EPOXY-POLYAMIDE, GREEN PRIMER, FORMULA 150, TYPE

III IN ACCORDANCE WITH MIL-DTL-24441 AND MIL-DTL-24441/20B (0.002" TO 0.003" DRY FILM THICKNESS).

D. INSPECT PART/ASSEMBLY FOR VOIDS. IF PRESENT USE COMPATIBLE EPOXY RESIN

MIXED WITH 410 MICROLIGHT FAIRING FILLER IN ACCORDANCE WITH

MANUFACTURERS (WEST SYSTEM, CAGE CODE 7S147) INSTRUCTIONS TO

FILL THE VOIDS. ALLOW TO DRY IN ACCORDANCE WITH MANUFACTURERS

INSTRUCTIONS AND SAND TO A UNIFORM FINISH. REPEAT STEPS C AND D

AS NECCESSARY TO FILL VOIDS.

E. THIRD AND FOURTH COAT: POLYURETHANE, AIRCRAFT AND SUPPORT EQUIPEMENT

IN ACCORDANCE WITH MIL-PRF-85285D, TYPE II, COLOR 26270 (HAZE GRAY) IN

ACCORDANCE WITH FED-STD-595 (0.001" TO 0.0015" DRY FILM THICKNESS).

THE TOTAL DRY FILM THICKNESS SHALL BE 0.007" TO .010".95.

DO NOT PAINT INSIDE OF RADOME.

4. MARK PART NUMBER 07609-93520, APPLICABLE DASH NUMBER,

AND "FSS" LOCATED APPROXIMATELY WHERE SHOWN IN .25 HIGH

GOTHIC CHARACTERS USING EPOXY MARKING INK, FIND NO. 11,

IN ACCORDANCE WITH MIL-STD-130.

5. SCAN ALL FSS PANELS (FRONT AND BACK), INCLUDING EDGES, TO INSURE A HOMOGENOUS

PATTERN AS SHOWN IN DETAIL D ON SHEET 3. TRIM AS NECESSARY.

FOR EACH COMPLETE RADOME (2 HALVES) CHECK EACH FSS PANEL ON BOTH SIDES AS SHOWN

IN DETAIL "D" AT PANEL CENTER AND 4 CORNERS APPROXIMATELY 1 INCH FROM EDGES. AT

EACH LOCATION MEASURE ALL DIMENSIONS AS SHOWN IN DETAIL "D" AT 4 ADJACENT TRACES.

IF CENTER MEASURMENTS ARE NOT WITHIN THE GIVEN LIMITS, THE PANEL MUST BE REJECTED.

IF ANY EDGE MEASUREMENTS ARE NOT WITHIN THE LIMITS, TRIM THE EDGES UNTIL THE

MEASUREMENTS ARE WITHIN THE LIMITS. ALL MEASUREMENTS TO BE TAKEN AT TRACE BASE

(INTERFACE OF TRACE AND FIBERGLASS SUBSTRATE) WITH AT LEAST 100X MAGNIFICATION AND OBLIQUE OR BACK LIGHTING. END OF TRACES WILL HAVE RADII OF .001-.002. TABULATE MEASURED

DATA IN CONTRACTORS FORMAT AND SUBMIT WITH EACH RADOME. SUBMIT ONE FSS SAMPLE

CUT FROM EACH PANEL USED IN RADOME AND LABEL APPROXIMATE LOCATION WHERE PANEL

WAS INSTALLED. SUBMIT EACH PACKET (ALL SAMPLE CUTS) WITH LOT NUMBER OF FSS MATERIAL

AND RADOME SERIAL NUMBER.

6. DRAFT ANGLE 1 MAX OVER THIS DIMENSION.

7. MATERIAL: G-10 .250 THICK PER MIL-I-24768.

8. MATERIAL: G-10 .375 THICK PER MIL-I-24768

9. INTERPRET DIMENSIONS AND TOLERANCING IAW Y14.5M-1994.

10. HONEYCOMB, FIND NO. 5 SHALL NOT BE COMPRESSED (DEFORMED FROM NATURAL SHAPE)

IN ANY WAY THROUGHOUT THE ENTIRE RADOME.

11. APPLY EPOXY, FIND NO. 10 AND FIND TO THE INTERAL SURFACE ON AND AROUND THE AREA OF ALL THREADED INSERTS (FIND NO. 1). COVER THE TOP, SIDES, AND GAP REMAINING FROM THE DRILLED HOLE AFTER ASSEMBLY TO

PREVENT LEAKS AROUND THE CIRCURFERENCE DURING PRESSURE TESTS.

12. APPLY EPOXY, FIND NO. 10 AND FIND NO. 11 TO THE CORNER TO CREATE A .125" RADIUS.

AS-

4127A/URC-

107(V) 93523

09-10-06STR

09-10-06D. MASON

DISTRIBUTION STATEMENT D. DoD AND THEIR

CONTRACTORS, NSWCDD, ANTENNA PRODUCTION

AND TESTING FACILITY, BUILDING 1530.

.31

.85

.48

.88

1.38

4.88

9.50

14.13

18.38 17.88

3X .50

SECTION B-B

8 10 11

1 14

.31 .03

.03.25

.03

1.00

1.00

1 LAYER

ALL AROUND

END JOINT

10 ALL AROUND

END JOINT

SECTION C-C

SCALE: 3/4

2 PLACES

FROM SHEET 1, ZONE C3

4 3

(FN 5)

(FN 2 AND FN 3)

.125

.110

.05 GLASS/EPOXY

.001 FSS

.001 FSS

.01 G-10

.05 GLASS/EPOXY

.56

.03 GLASS/EPOXY

SEE DETAIL D, SH3

.001 FSS

.01 G10

.001 FSSS

.03 GLASS/EPOXY

.25 HONEYCOMB

.25 HONEYCOMB

DETAIL E

R .25 TYP

R .25 TYP

SECTION G-G

SCALE: 1/2

FROM SHEET 1, ZONE C5

12. AR 2X12. 2X

5 REQD 2 3

5 REQD

SCALE: 1/4

MIRRORED ON OPPOSITE SIDE

FROM SHEET 1, ZONE C5 SCALE: 1/1

FROM SHEET 1, ZONE D2

AR

7 8

07609 93520 N/A 2

93520 2

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E

DISTRIBUTION STATEMENT D. DoD AND THEIR

CONTRACTORS, NSWCDD, ANTENNA PRODUCTION

AND TESTING FACILITY, BUILDING 1530.

.25

.54

R17.89

R17.13

R13.85

.44

.38

1.00

.54

.0035 .0041

.0041

.0035 (GAP)

.0035 .0041

.0296 .0308

(TRACE LENGTH)

.1222

.1190

(STAGGER)

-101

SUPPORT RING

MATERIAL: MIL-I-24768/2 G-10

.25 THICK

SCALE: 1/4

-102

INSERT MOUNTING BLOCK

MATERIAL: MIL-I-24768/2 G-10

.38 THICK

SCALE: 2/1

FSS FACING OUTSIDE

FSS FACING INSIDE

(VERTICAL ONLY AT CENTER OF RADOME)

(ETCHING DIMENSIONS SAME AS OUTSIDE)

DETAIL D

SCALE 60:1

DARK AREAS ARE COPPER TRACES

INSIDE/OUTSIDE ETCHING TRACE ALIGNMENT 90 5

ALIGN END GAP AT CENTER OF VERTICAL PATTERN WITH END GAP AT CENTER OF HORIZONTAL PATTERN

DIMENSIONS ARE TAKEN AT BASE OF TRACE

(END GAP)

(TRACE WIDTH)

07609 93520

NA 3

93520 3

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