Antenna Foundation diagram.pdf

PDF 265 KB Posted

Attached to
DET C Guam Antenna Federal contract opportunity
Solicitation number
FA251825R0017
Issued by
Department of the Air Force Space Command

About this file

This technical drawing is a detailed foundation plan for a 9.1-meter low-profile satellite antenna system, specifically designed for a Viasat installation. The document provides comprehensive specifications for the antenna foundation, including critical loading parameters and installation requirements. Key technical details include maximum wind load tolerances (drive to stow wind at 65 MPH, survival wind at 125 MPH), a maximum dead load of 71,200 lbs, and an operating temperature range of -40°F. The foundation plan specifies a circular mounting configuration with 36 anchor bolts, requiring precise vertical alignment within 1/64 inch per inch and a concrete pad surface level within 0.25 inches. The document emphasizes the importance of professional engineering services for foundation design, noting that local building codes and environmental conditions must be carefully considered during installation. The foundation is designed to support a 3-axis (EL/AZ/Train) antenna system with a specified elevation axis height of 284 inches from the foundation interface plane.

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Text version

ϴ 7

OVERTURNING MOMENT

CENTER OF GRAVITY

ANTENNA CENTERLINE

FOUNDATION

MOUNTING STUD

TORSION LOAD

HORIZONTAL SHEAR LOAD

STUD TENSILE LOAD

STUD SHEAR LOAD

ORIGIN

DEAD LOAD

THIS TECHNICAL DATA IS SUBJECT TO THE UNITED STATES EXPORT ADMINISTRATION

REGULATIONS. DIVERSION CONTRARY TO US LAW IS PROHIBITED.

5.0°±1.0°

36X 10.0°

84.00 DBC

94.0

92.0 5

A A

TRUE NORTH 1.0

REF

(36X 1"-8 UNC-2A STUD)

.112 A B C

C B

36X 8.0±.2 ANCHOR BOLT

PROJECTION

3.0 MIN

CLEARANCE

TO ANY REBAR

SECTION A-A 1

REF

REF 2

A5

IMPORTANT NOTICE

VIASAT DOES NOT REPRESENT, NOR RECOMMEND THAT ANY

PARTICULAR DESIGN OR SIZE OF FOUNDATION OR STUD IS

APPROPRIATE FOR ANY PARTICULAR LOCATION OR INSTALLATION.

SINCE SOIL AND ENVIRONMENTAL CONDITIONS, BUILDING CODES,

INSTALLATION PRACTICES, AND OTHER FACTORS VARY AMONG

DIFFERENT LOCALITIES, THOSE PERSONS INSTALLING ANTENNA

MOUNTS ARE CAUTIONED TO SECURE PROFESSIONAL

ENGINEERING SERVICES FOR THE DESIGN AND CONSTRUCTION

SUPERVISION OF ANTENNA MOUNT FOUNDATION.

INTERPRET DIMENSIONING AND TOLERANCES PER ASME Y14.5-2018.

ALL FOUNDATION CONSTRUCTION AND DETAILS SHALL BE PER LOCAL

CODES AND REGULATIONS. SLAB SHOWN IS FOR REFERENCE ONLY. SLAB

SIZE AND SHAPE SHALL BE DETERMINED BY CONTRACTOR TO MEET

FOUNDATION LOADING REQUIREMENTS LISTED IN THE FOUNDATION

LOADING TABLE ON THIS SHEET. SEISMIC LOADING IS NOT CONSIDERED

SIMULTANEOUS WITH WIND AND ACCELERATION LOADING.

USE PROVIDED VIASAT ANCHOR BOLT TEMPLATES TO ESTABLISH ANCHOR

BOLT SPACING DURING FOUNDATION CONSTRUCTION. THE TEMPLATES

AND STUD SUBASSEMBLY SHOWN ON SHEET 2 SHOULD BE SUPPORTED

BY A RIGID STRUCTURE TO MAINTAIN ANCHOR STUD VERTICALITY.

ANCHOR BOLTS SHALL NOT BE WELDED.

MAXIMUM FOUNDATION COMPLIANCE IS LISTED IN THE LOADING TABLE.

COMPLIANCE IS ANALYZED ACROSS THE BOLT PATTERN ONLY WITH

LOADING APPLIED TO THE BOLTS. THE FOUNDATION UNDER ALL LOADS

MUST BE STABLE IN ALL SEASONS INCLUDING FROST LINE, MOISTURE,

AND OTHER SOIL CONDITIONS.

SURFACE OF CONCRETE PAD INSIDE OF DESIGNATED AREA SHALL BE

LEVEL WITHIN 0.25 INCH. OUTSIDE OF DESIGNATED AREA SHALL BE

DESIGNED FOR PROPER DRAINAGE AWAY FROM THE ANTENNA. STUDS

AND AREA AROUND STUDS SHALL BE FREE OF CONCRETE BUILD UP. IF

GROUT IS REQUIRED, THE PAD SURFACE AROUND THE BOLT PATTERN

SHALL BE LEFT ROUGH FOR GOOD GROUT BOND.

1.

NOTES:

MOUNTING STUDS ARE PROVIDED FOR CONVIENENCE. STUD LENGTH TO

BE DETERMINED BY CONTRACTOR PER FOUNDATION ANALYSIS. IT IS

CRITICAL TO ANALYZE THE STUDS AS PART OF THE DESIGN TO ASSURE

LENGTH PROVIDED IS ADEQUATE FOR THE SITE. SEE DETAIL ON SHEET 2

FOR DIMENSIONS OF THE HARDWARE PROVIDED. ANTENNA MOUNTED

DIRECTLY ON TOP OF THE FOUNDATION.

COMPLIANCE IS DEFINED AS THE RATIO OF THE AMOUNT OF TILT OF THE

FOUNDATION, ϴ, TO THE OVERTURNING MOMENT THAT IS APPLIED TO IT.

EXPRESSED IN RAD/FT-LB.

THE RADOME RING WALL, IF INCLUDED, SHALL BE ISOLATED FROM THE

PEDESTAL FOUNDATION SUCH THAT WIND AND TEMPERATURE LOADS ON

THE RADOME ARE NOT IMPARTED ON THE PEDESTAL FOUNDATION.

FOUNDATION COMPLIANCE APPLIES ONLY TO PEDESTAL FOUNDATION

PAD.

THIS DOCUMENT MUST BE USED IN CONJUNCTION WITH THE PROGRAM

LEVEL INTERFACE CONTROL DOCUMENT (ICD) TO DETERMINE VIASAT'S

FULL REQUIREMENTS. SEE THE PROGRAM LEVEL ICD FOR SPECIFICS ON:

-ANTENNA SYSTEM PHYSICAL ENVELOPE AND REQUIRED CLEARANCE

-ELECTRICAL GROUNDING AND LIGHTNING PROTECTION

-ELECTRICAL POWER

-INDOOR EQUIPMENT

-CABLE MANAGEMENT FEATURES (CONDUITS, TROUGHS, ETC.)

-GROUTING (IF APPLICABLE)

-RADOME AND RING WALL (IF APPLICABLE)

-OTHER PROGRAM SPECIFIC REQUIREMENTS

9.

2 4 7 8FOUNDATION LOADING TABLE

WIND LOADS:

MAX OVERTURNING MOMENT: 355,000 FT-LBS [484 kNm] MAX TORSION LOAD: 55,000 FT-LBS [75 kNm] HORIZONTAL SHEAR LOAD: 14,100 LBS [63 kN] MAX ANCHOR STUD TENSILE LOAD: 5,700 LBS [25.4 kN] MAX ANCHOR STUD SHEAR LOAD: 400 LBS [1.8 kN]

MAX FOUNDATION COMPLIANCE

PEDESTAL FOOTPRINT 8 : 1.0 X 10E-9 RAD/FT-LB

LOADING BASED ON FOLLOWING PARAMETERS:

ANTENNA SYSTEM: 3-AXIS (EL/AZ/TRAIN)

REFLECTOR: 9.1 M

EL AXIS HEIGHT FROM RISER-FOUNDATION INTERFACE PLANE: 284 INCH [7.21 M]

MAX DEAD LOAD: 71,200 LBS [317 kN]

DEAD LOAD HEIGHT: 265 INCH [6.73 M]

MAXIMUM ALLOWABLE WIND:

DRIVE TO STOW WIND: 65 MPH [105 KPH]

SURVIVAL WIND STOWED AT ZENITH: 125 MPH [200 KPH]

TEMPERATURE: -40 F [-40 C]

CALCULATED AT WORST CASE WIND APPROACH ANGLE

(USE SAME LOADING FOR 2-AXIS EL/AZ SYSTEM)

FOUNDATION PLAN, 3440

LOW, 9.1 M

SHEET 1 OF 2

CAGE CODE

TITLE

SCALE:

DRAWING NO.SIZE

D

REV

OWNER

CAD GENERATED DRAWING: SOLIDWORKS

TEMPLATE P/N: 1236498 REV 002

D

C

B

A

345678

A

B

C

D

45678

2022/06/13

NONE

Brown, Arthur

PROPRIETARY NOTICE

THESE DRAWINGS, LISTS OR SPECIFICATIONS ARE THE

CONFIDENTIAL INFORMATION AND/OR TRADE SECRETS

OF VIASAT, INC., AND ISSUED IN STRICT CONFIDENCE.

EXCEPT AS AUTHORIZED BY VIASAT IN WRITING, THESE

DRAWINGS, LISTS OR SPECIFICATIONS SHALL NOT BE

REPRODUCED, RETRANSMITTED, USED FOR THE DESIGN,

MANUFACTURE OR SALE OF EQUIPMENT OR USED FOR

ANY OTHER PURPOSE OTHER THAN EVALUATION.

3 2

ELECTRONIC APPROVALS

ON FILE IN AGILE

LBS

FINISH

THIRD ANGLE PROJECTION

WT:

DATE(YYYY/MM/DD)

DO NOT SCALE DRAWING

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES AND APPLY

AFTER FINISH OR PLATING. TOLERANCES ARE:

MAX SURFACE ROUGHNESS 125 MICRO-IN ON

ALL MACHINED SURFACES EXCEPT AS NOTED.

BREAK SHARP EDGES AND CORNERS .010 MAX.

.X .XX .XXX .XXXX ANGULAR

±.1 ±.02 ±.005 ±.0005 ±.5°

DRILLED HOLE DIAMETER

CONTRACT NO.

00214219511Q601

.000-.250 .251-.500 .501-1.000 1.001-1.500 +.004 +.006 +.007 +.010 -.001 -.001 -.001 -.001

1725 BRECKINRIDGE PLAZA

DULUTH, GA 30096

REVISION HISTORY IN AGILE (ALL SHEETS AT SAME REVISION)

REV DESCRIPTION ELECTRONIC SIGNATURES

ON FILE IN AGILECO-002 224014

4 PL

ANCHOR BOLT AND TEMPLATE

SUBASSEMBLY DETAIL

3 2 PL

36 PL

MIN 7.0 OF

THREAD

1-8 UNC-2A

(36.0)

.75

MIN 3.0 OF

THREAD

1-8 UNC-2A 4.0

8.0 6.8

1.8

ANCHOR BOLTS ABOVE CONCRETE

MUST BE VERTICAL WITHIN 1/64 INCH/INCH

TOP OF CONCRETE

NOT TO SCALE

36 PLACES

REF

REF

REF

ANCHOR BOLT FURNISHED

BY VIASAT

REF

REF

REF

ANCHOR BOLT

DETAIL

2 PL

2 PL

SHEET 2

CAGE CODESIZE

D

REV

D

C

B

A

345678

A

B

C

D

45678

3 2

DRAWING NO.

NONESCALE:

1Q601 1421951

THIS TECHNICAL DATA IS SUBJECT TO THE UNITED STATES EXPORT ADMINISTRATION

REGULATIONS. DIVERSION CONTRARY TO US LAW IS PROHIBITED.

Sheet1
Drawing View1
Section View A-A
Sheet2
Drawing View8
Drawing View9

File details come from the government source that posted it. Updated .