NFRC U-FACTOR, SHGC, VT, &CONDENSATION RESISTANCE

COMPUTER SIMULATION REPORT

Rendered to:TUBELITE, INC.

SERIES/MODEL:Thermal Door w/ T24000 Framing

Report Number:Report Date:

C5869.03-116-4511/06/13

Architectural Testing

130 Derry Court York, PA 17406-8405 phone: 717-764-7700 fax: 717-764-4129 www.archtest.com

NFRC U-FACTOR, SHGC, VT, & CONDENSATION RESISTANCECOMPUTER SIMULATION REPORT

Rendered to:TUBELITE, INC.

4878 Mackinaw TrailReed City, Michigan 49677

Report Number:Simulation Date:

Report Date:

Project Summary:

Standards:

Software:

Simulations Specimen Description:Series/Model: Thermal Door w/ T24000 FramingType: Swinging Door, Single Leaf Entrance Door Frame Material: AP Aluminum w/ Thermal Breaks - Partial Sash Material: AT Aluminum w/ Thermal Breaks - All Members Standard Size: 960mm x 2090mm

C5869.03-116-4511/06/1311/06/13

Architectural Testing, Inc. was contracted to perform U-Factor, Solar Heat Gain Coefficient,Visible Transmittance, and Condensation Resistance* computer simulations in accordance withthe National Fenestration Rating Council (NFRC). The products were evaluated in fullcompliance with NFRC requirements to the standards listed below.

*NFRC's Condensation Resistance rating is NOT equivalent to a Condensation ResistanceFactor (CRF) determined in accordance with AAMA 1503.

NFRC 100-2010: Procedure for Determining Fenestration Product U-FactorsNFRC 200-2010: Procedure for Determining Fenestration Product Solar Heat Gain

Coefficient and Visible Transmittance at Normal IncidenceNFRC 500-2010: Procedure for Determining Fenestration Product Condensation

Resistance Values

Frame and Edge Modeling: THERM 6.3.46Center-of-Glass Modeling: WINDOW 6.3.74Total Product Calculations: WINDOW 6.3.74Spectral Data Library: IGDB 32.0

Architectural Testing

130 Derry Court York, PA 17406-8405 phone: 717-764-7700 fax: 717-764-4129 www.archtest.com

C5869.03-116-45Page 2 of 7

Modeling Assumptions/Technical Interpretations:1) To prevent air infiltration, tape was applied to all interior sash crack locations.2) This product is available in either a painted or anodized finish. These two finish

types were grouped for simulation purposes in accordance with NFRC 100-2010, Section 4.2.1.L. The painted finish was simulated since it is worst case (highestemissivity).

Specialty Products Table:

SHGC = SHGC0 + SHGCc (SHGC1 - SHGC0)VT = VT0 + VTc (VT1 - VT0)

Validation Matrix:

The specialty products method allow the manufacturer to determine the overall product SHGCand VT for any glazing option. The center of glass SHGC and/or VT must be determined usingWINDOW 6.3.74. The method gives overall product SHGC and VT indexed on center of glassproperties. All values used in the calculations are truncated to six decimal place precision.

No Dividers Dividers < 1 Dividers > 1SHGC0 0.031627 0.034126 0.036412SHGC1 0.508259 0.434361 0.380321VT0 0.000000 0.000000 0.000000VT1 0.476633 0.400236 0.330350

The following products are part of a validation matrix. Only one is required for validationtesting.

Product Line Report NumberNone -

Architectural Testing

C5869.03-116-45Page 3 of 7

Spacer Option Description

Grid Option Description

Reinforcement Option Description

Gas Filling Technique Description

Edge-of-Glass Construction

Weatherstripping

Frame/Sash Materials Finish

SealantSpacer Type Primary Secondary CodeAluminum Dual Seal Spacer Butyl Rubber Butyl Rubber A1-D

Grid Size Grid Type Grid PatternNone - -

Location MaterialNone -

Fill Type Method84.48% Xenon Single Probe Timed

Interior Condition EPDM Gasket Between Aluminum Glazing Bead and GlassExterior Condition EPDM Gasket Between Aluminum Glazing Bead and Glass

76.14% Argon Single Probe Timed88.47% Argon Single Probe Timed

Type Quantity LocationBulb Weatherseal 1 Row Head and Jamb FramesConcealed Screw Weatherstrip 1 Row Sill Frame

Interior Painted AluminumExterior Painted Aluminum

78.56% Argon Single Probe Timed78.10% Krypton Single Probe Timed87.41% Argon Single Probe Timed64.98% Argon Single Probe Timed74.70% Argon Single Probe Timed60.78% Argon Single Probe Timed62.43% Argon Single Probe Timed86.02% Argon Single Probe Timed81.60% Xenon Single Probe Timed94.54% Xenon Evacuated Chamber

71.54% Xenon Single Probe Timed76.45% Krypton Single Probe Timed66.67% Xenon Single Probe Timed82.16% Xenon Single Probe Timed

76.90% Krypton Single Probe Timed

Architectural Testing

C5869.03-116-45Page 4 of 7

NFRC 100/200/500 Summary SheetThermal Door w/ T24000 Framing

ID

Pane

Thi

ckne

ss 1

Gap

Wid

th 1

Pane

Thi

ckne

ss 2

Gap

Wid

th 2

Pane

Thi

ckne

ss 3

Gap

Wid

th 3

Pane

Thi

ckne

ss 4

Gri

d T

ype

U-FactorSolar Heat Gain Coefficient (SHGC)

Grids (None / <1 / >=1)

Visible Transmittance (VT)Grids (None / <1 / >=1)

Gap

Fill

Low

-e (S

urfa

ce#)

Tin

t

Spac

er

A1-D N

CondensationResistance

1 COG=0.44000.222 0.500 0.225

VT (N) 0.35

XEN84 CLU-Factor 0.64 SHGC (N) 0.36

A1-D N

CR 37

2 COG=0.42000.236 0.500 0.225

VT (N) 0.15

ARG76 0.654(#2) RCU-Factor 0.63 SHGC (N) 0.20

A1-D N

CR 37

3 COG=0.40000.223 0.500 0.225

VT (N) 0.08

ARG88 0.571(#2) CLU-Factor 0.62 SHGC (N) 0.14

A1-D N

CR 37

4 COG=0.38000.236 0.500 0.225

VT (N) 0.07

ARG79 0.465(#2) RCU-Factor 0.61 SHGC (N) 0.13

A1-D N

CR 38

5 COG=0.36000.221 0.500 0.225

VT (N) 0.09

KRY78 0.406(#2) SRU-Factor 0.60 SHGC (N) 0.13

A1-D N

CR 38

6 COG=0.34000.232 0.500 0.225

VT (N) 0.27

ARG87 0.318(#2) GYU-Factor 0.59 SHGC (N) 0.25

A1-D N

CR 38

7 COG=0.32000.223 0.500 0.225

VT (N) 0.35

ARG65 0.215(#2) CLU-Factor 0.59 SHGC (N) 0.33

A1-D N

CR 38

8 COG=0.30000.233 0.500 0.225

VT (N) 0.25

ARG75 0.166(#2) CLU-Factor 0.58 SHGC (N) 0.24

A1-D N

CR 38

9 COG=0.28000.223 0.500 0.225

VT (N) 0.36

ARG61 0.087(#2) CLU-Factor 0.57 SHGC (N) 0.29

A1-D N

CR 38

10 COG=0.26000.223 0.500 0.225

0.21 VT (N) 0.33

ARG62 0.035(#2) CLU-Factor 0.56 SHGC (N) CR 38

Architectural Testing

C5869.03-116-45Page 5 of 7

Gap

Wid

th 1

Pane

Thi

ckne

ss 2

Gap

Wid

th 2

Pane

Thi

ckne

ss 3

Gap

Fill

Low

-e (S

urfa

ce#)

Tin

t

Spac

er

NFRC 100/200/500 Summary SheetThermal Door w/ T24000 Framing

ID

Pane

Thi

ckne

ss 1

Gri

d T

ype

U-FactorSolar Heat Gain Coefficient (SHGC) Visible Transmittance (VT) Condensation

Grids (None / <1 / >=1) Grids (None / <1 / >=1) Resistance

Gap

Wid

th 3

Pane

Thi

ckne

ss 4

11 COG=0.24000.223 0.500 0.223 ARG86U-Factor 0.55 SHGC (N) 0.20 VT (N) 0.30

0.035(#2) / 0.035(#3) CL A1-D N

A1-D N

CR 38

12 COG=0.22000.223 0.500 0.223

VT (N) 0.25

XEN82 0.018(#2) / 0.018(#3) CLU-Factor 0.54 SHGC (N) 0.15

A1-D N

CR 38

13 COG=0.20000.223 0.500 0.223

VT (N) 0.25

XEN95 0.018(#2) / 0.018(#3) CL

0.221

U-Factor 0.53 SHGC (N) 0.15

A1-D N

CR 38

14 COG=0.18000.223 0.250 0.003 0.250

VT (N) 0.21

KRY77/AIR 0.018(#2)/0.755(#3)/0.122(#4)/0.028(#5) CL

0.223

U-Factor 0.52 SHGC (N) 0.15

A1-D N

CR 38

15 COG=0.16000.223 0.250 0.003 0.250

VT (N) 0.22

XEN72/AIR 0.018(#2, #5) / 0.755(#3) / 0.122(#4) CL

0.223

U-Factor 0.51 SHGC (N) 0.15

A1-D N

CR 38

16 COG=0.14000.223 0.250 0.003 0.250

VT (N) 0.22

KRY76 0.018(#2, #5) / 0.755(#3) / 0.122(#4) CL

0.223

U-Factor 0.51 SHGC (N) 0.14

A1-D N

CR 38

17 COG=0.12000.223 0.250 0.003 0.250

VT (N) 0.22

XEN67 0.018(#2, #5) / 0.755(#3) / 0.122(#4) CL

0.223

U-Factor 0.50 SHGC (N) 0.14

A1-D N

CR 38

18 COG=0.10000.223 0.250 0.003 0.250

VT (N) 0.22

XEN82 0.018(#2, #5) / 0.755(#3) / 0.122(#4) CLCR 38U-Factor 0.49 SHGC (N) 0.14

Architectural Testing

C5869.03-116-45Page 6 of 7

SIMULATED BY: REVIEWED BY:

Kristen L. Livelsberger Michael J. ThomanSenior Simulation Technician Director - Simulations and Thermal TestingNFRC Certified Simulator Simulator-In-Responsible-Charge

KLL:kllC5869.03-116-45

Attachments (pages): This report is complete only when all attachments listed are included.Appendix A: Drawings and Bills of Material (37)

The Condensation Resistance results obtained from this procedure are for controlled laboratoryconditions and do not include the effects of air movement through the specimen, solar radiation, and the thermal bridging that may occur due to the specific design and construction of thefenestration system opening.

Ratings values included in this report are for submittals to an NFRC-licensed IA and are notmeant to be used directly for labeling purposes. Only those values identified on a validCertification Authorization Report (CAR) by an NFRC accredited Inspection Agency (IA) areto be used for labeling purposes. The ratings values were rounded in accordance to NFRC 601,NFRC Unit and Measurement Policy.

Architectural Testing, Inc. is an NFRC accredited simulation laboratory and all simulationswere conducted in full compliance with NFRC approved procedures and specifications. TheNFRC procedure requires that the computational results be verified through actual test results.

Architectural Testing will service this report for the entire test record retention period. Testrecords that are retained such as detailed drawings, datasheets, representative samples of testspecimens, or other pertinent project documentation will be retained by Architectural Testing,Inc. for the entire test record retention period. The test record retention end date for this reportis November 6, 2017.

Results obtained are simulated values and were secured by using the designated test methods.This report does not constitute certification of this product nor an opinion or endorsement bythis laboratory. It is the exclusive property of the client so named herein and relates only to theproduct simulated. This report may not be reproduced, except in full, without the writtenapproval of Architectural Testing, Inc.

For ARCHITECTURAL TESTING, INC.:

Architectural Testing

C5869.03-116-45Page 7 of 7

Revision Log

Rev. # Date Page(s) Revision(s)

This report produced from controlled document template ATI 00037, Revised 10/2/2012.

.03R0 11/06/13 All Original Report Issued to Tubelite, Inc.

Architectural Testing

All drawings and Bills of Material used to simulate this product are enclosed in this Appendix

Appendix AC5869.03-116-45

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