Antenna Foundation diagram.pdf
PDF 265 KB Posted
- Attached to
- DET C Guam Antenna Federal contract opportunity
- Solicitation number
- FA251825R0017
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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| Solicitation Amendment 3 FA251825R00170003 SF 30.pdf | ||
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| Davis Bacon Act WD GU20250001 01032025.pdf | ||
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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 |
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