08-20013_BOOM FAILSAFE package.pdf

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Mobile Launch Vehicle (MLV) Fabrication
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This document is a comprehensive technical drawing package for a Boom Failsafe assembly (part number 08-20013) for the NASA Balloon Program. The assembly consists of four nested telescoping boom stages with integrated fail-safe mechanisms, designed to extend from a stowed configuration of 98.25 inches to a maximum extension of 254.75 inches. The complete system weighs approximately 1,059.3 pounds and is constructed primarily from shaped A500 Grade C steel with selected components in 316 stainless steel and AISI 1045 steel.

The boom failsafe assembly comprises 28 primary components including four nested tubular stages (items 1-4), a foot assembly (item 5), 38 internal slides (item 6), wedge blocks, spring pin plungers with upper and lower spring pin bodies, tapered pins, hydraulic cylinders with 4.9-ton capacity and 3.11-inch stroke, body and plunger end eyes, dowel pins, cotter pins, and various fasteners. All welding must comply with AWS D1.1/D1.1M:2020 standards with visual and magnetic particle or liquid penetrant testing required. Post-weld finishing includes surface preparation per NASA-STD-5008B §4.4.2, application of Carboline Carbozinc 11 WB primer, Carboacrylic 3358 midcoat (brown), and minimum two coats of Carboacrylic 3359 topcoat (black, color code C900 or equivalent FED-STD-595 No. 17038). All fasteners require MIL-PRF-907H Type II graphite/aluminum anti-seize compound application with specific torque values: M4×0.7 (3 ft-lbs), M6×1.0 (13 ft-lbs), and M10×1.5 (25 ft-lbs).

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Text version

ISOMETRIC STOWED POSITION

FOR REFERENCE ONLY

NOTES (UNLESS OTHERWISE SPECIFIED):

ALL DIMENSIONS IN INCHES UNLESS OTHERWISE1.

SPECIFIED

CHASE ALL THREADS BEFORE INSTALLING FASTENERS2.

APPLY MIL-PRF-907H TYPE II GRAPHITE/ALUMINUM3.

ANTI-SEIZE COMPOUND TO THREAD AND SHANK OF

ALL FASTENERS AND TORQUE ALL FASTENERS PER

TORQUE TABLE UNLESS OTHERWISE SPECIFIED.

A

DATE REV. DESCRIPTION ENG/DFT

9/24/2024 - ORIGINAL RELEASE KWS

10/16/2024 A CHANGED ITEM 22 FROM 45MM CLASS 8.8 TO 60MM

CLASS 12.9 PER CR 2752 KWS

ALL FASTENERS SHALL HAVE A FRICTION FACTOR OF .18

USED (FASTENERS LUBRICATED W/ MIL-PRF-907H

ANTISEIZE COMPOUND).

SIZE AND THREAD TORQUE VALUE

(FT-LBS[NM])

M4 X 0.7 3 [4] M6 X 1.0 13 [17] M10 X 1.5 25 [33]

Item No. QTY PART No. DESCRIPTION SOURCE SOURCE PART No.

1 1 08-20013-100 STAGE 1, BOOM FAILSAFE, NBOC MLV

2 1 08-20013-02 STAGE 2, BOOM FAILSAFE, NBOC MLV

3 1 08-20013-03 STAGE 3, BOOM FAILSAFE, NBOC MLV

4 1 08-20013-200 STAGE 4, BOOM FAILSAFE, NBOC MLV

5 1 08-20013-500 FOOT, BOOM FAILSAFE, NBOC MLV

6 38 08-20013-04 INTERNAL SLIDE, BOOM FAILSAFE, NBOC MLV

7 4 08-20013-01 WEDGE BLOCK, BOOM FAILSAFE, NBOC MLV

8 2 08-20013-300 SPRING PIN PLUNGER, BOOM FAILSAFE, NBOC MLV

9 1 08-20013-400 LOWER SPING PIN BODY, BOOM FAILSAFE, NBOC MLV

10 4 08-20013-05 TAPERED PIN, BOOM FAILSAFE, NBOC MLV

11 1 ERS LINEAR COIL SPRING, 5 IN LENGTH, 105 LBF/IN EIBACH 0500.163.0105

12 1 ERS LINEAR COIL SPRING, 6 IN LENGTH, 105 LBF/IN EIBACH 0600.188.0105

13 1 08-20013-600 UPPER SPRING PIN BODY, BOOM FAILSAFE, NBOC MLV

14 2 BODY END EYE, FOR 5 TON CYLINDERS ENERPAC REB5

15 2 PLUNGER END EYE, FOR 5 TON CYLINDERS ENERPAC REP5

16 2 4.9 TON CAPACITY, 3.11" STROKE, GENERAL PURPOSE HYDRAULIC CYLINDER ENERPAC RC53

17 4 .625 X 1.25, 316 STAINLESS PIN MCMASTER-CARR 92056A227

18 38 10MM DIA, 12MM LENGTHM DOWEL PIN 4140 ALLOY MCMASTER-CARR 91595A166

19 4 FOR .625 PIN, .125 WIRE, COTTER PIN, ZINC PLATED MCMASTER-CARR 98335A074

20 76 M4X0.7MM, 12MM, FHS, CLASS 10.9, ZINC PLATED MCMASTER-CARR 91263A829

21 8 M10X1.5MM, 18MM, HHCS, CLASS 8.8, ZINC PLATED MCMASTER-CARR 91280A982

22 12 HEX HEAD SCREW, M10X1.5 X 60MM, CLASS 12.9, ZINC PLATE YELLOW

CHROMATE MCMASTER-CARR 91029A116

23 32 M10 ZINC PLATED CLASS 10.9 STANDARD WASHER MCMASTER-CARR 91455A613

24 12 M10X1.5MM, LOCKNUT, ZINC PLATED, CLASS 10 MCMASTER-CARR 94645A220

25 4 M6X1MM, 25MM, SHCS, CLASS 12.9, ZINC PLATED MCMASTER-CARR 90128A265

26 2 08-20018-10 ROLLER SWITCH ASSEMBLY, NBOC MLV

27 4 M4X0.7MM, 40MM, SHCS, 18-8 STAINLESS MCMASTER-CARR 91292A132

28 2 08-20021 SPRING LOCKING PIN ASSEMBLY, NBOC MLV

TOLERANCE (INCH)

C

INTERPRET PER ASME Y14.5-2009

X.X

X.XX

X.XXX

125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

CAGE CODE

APPROX. WEIGHT

1059.3

THIRD ANGLE PROJECTION SCALE:

1:10

DO NOT SCALE

FROM DRAWING

N/A

MATERIAL:

NBOC MLV

PROJECT:

08-20001

NEXT ASSEMBLY:

BOOM FAILSAFE, NBOC MLV

TITLE:

DATE:

DES.

CHK.

DFT.

ENG.

08-20013 REV.

ASHEET 1 OF 7

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED

COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE OBTAINED FROM THE BUREAU OF INDUSTRY AND SECURITY, UNITED STATES

DEPARTMENT OF COMMERCE. VIOLATIONS OF THESE REGULATIONS ARE PUNISHABLE BY FINE,

IMPRISONMENT, OR BOTH.

REV 03/2024

.1

.02

.005

.25

A A

B B

C C

D D

E E

98.25

STOWED CONFIGURATION

254.75

MAX EXTENSION CONFIGURATION

TOLERANCE (INCH)

C

INTERPRET PER ASME Y14.5-2009

X.X

X.XX

X.XXX

125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

CAGE CODE

APPROX. WEIGHT

1059.3

THIRD ANGLE PROJECTION SCALE:

1:10

DO NOT SCALE

FROM DRAWING

N/A

MATERIAL:

NBOC MLV

PROJECT:

08-20001

NEXT ASSEMBLY:

BOOM FAILSAFE, NBOC MLV

TITLE:

DATE:

DES.

CHK.

DFT.

ENG.

08-20013 REV.

ASHEET 2 OF 7

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED

COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE OBTAINED FROM THE BUREAU OF INDUSTRY AND SECURITY, UNITED STATES

DEPARTMENT OF COMMERCE. VIOLATIONS OF THESE REGULATIONS ARE PUNISHABLE BY FINE,

IMPRISONMENT, OR BOTH.

REV 03/2024

.1

.02

.005

.25

A A

B B

C C

D D

E E

INSERT ALL STAGES INTO THE BOTTOM OF

STAGE 1 BEFORE INSTALLING ITEM 5

23 2X

21 2X

INSTALLED ON BOTH SIDES

28 2X

17 2X

17 2X

26 2X

16 2X

14 2X

15 2X

19 2X

27 4X

INSTALL ON ALTERNATING

CORNERS AND TORQUE

TO 18 IN-LBS [2NM]

22 12X

23 24X

24 12X

TORQUE INCLUDED FASTENERS TO 12 FT-LBS [16 NM]

19 2X

TOLERANCE (INCH)

C

INTERPRET PER ASME Y14.5-2009

X.X

X.XX

X.XXX

125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

CAGE CODE

APPROX. WEIGHT

1059.3

THIRD ANGLE PROJECTION SCALE:

1:4

DO NOT SCALE

FROM DRAWING

N/A

MATERIAL:

NBOC MLV

PROJECT:

08-20001

NEXT ASSEMBLY:

BOOM FAILSAFE, NBOC MLV

TITLE:

DATE:

DES.

CHK.

DFT.

ENG.

08-20013 REV.

ASHEET 3 OF 7

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED

COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE OBTAINED FROM THE BUREAU OF INDUSTRY AND SECURITY, UNITED STATES

DEPARTMENT OF COMMERCE. VIOLATIONS OF THESE REGULATIONS ARE PUNISHABLE BY FINE,

IMPRISONMENT, OR BOTH.

REV 03/2024

.1

.02

.005

.25

A A

B B

C C

D D

E E

11.5

A

A

23 2X

21 2X

82.75

11.5

B

B

SECTION A-A

TYP 2 PLACES

20 2X

SECTION B-B

TYP 2 PLACES

6 2X

20 4X

18 2X

TYP 2 PLACES

TOLERANCE (INCH)

C

INTERPRET PER ASME Y14.5-2009

X.X

X.XX

X.XXX

125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

CAGE CODE

APPROX. WEIGHT

303.3

THIRD ANGLE PROJECTION SCALE:

1:5

DO NOT SCALE

FROM DRAWING

N/A

MATERIAL:

NBOC MLV

PROJECT:

N/A

NEXT ASSEMBLY:

STAGE 1 ASSEMBLY, BOOM FAILSAFE,

NBOC MLV

TITLE:

DATE:

DES.

CHK.

DFT.

ENG.

08-20013 REV.

ASHEET 4 OF 7

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED

COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE OBTAINED FROM THE BUREAU OF INDUSTRY AND SECURITY, UNITED STATES

DEPARTMENT OF COMMERCE. VIOLATIONS OF THESE REGULATIONS ARE PUNISHABLE BY FINE,

IMPRISONMENT, OR BOTH.

REV 03/2024

.1

.02

.005

.25

A A

B B

C C

D D

E E

8.219

C

C

20 2X

8.219

84.0

D

D

6 2X

20 4X

18 2X

SECTION C-C

TYP 2 PLACES

20 2X

SECTION D-D

TYP 2 PLACES

6 2X

20 4X

18 2X

TYP 2 PLACES TYP 2 PLACES

TOLERANCE (INCH)

C

INTERPRET PER ASME Y14.5-2009

X.X

X.XX

X.XXX

125SURFACE FINISH IN

MICROINCHES RMS

CAGE CODE

APPROX. WEIGHT

259.3

THIRD ANGLE PROJECTION SCALE:

1:5

DO NOT SCALE

FROM DRAWING

N/A

MATERIAL:

NBOC MLV

PROJECT:

N/A

NEXT ASSEMBLY:

STAGE 2 ASSEMBLY, BOOM FAILSAFE,

NBOC MLV

TITLE:

DATE:

DES.

CHK.

DFT.

ENG.

08-20013 REV.

ASHEET 5 OF 7

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED

COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE OBTAINED FROM THE BUREAU OF INDUSTRY AND SECURITY, UNITED STATES

DEPARTMENT OF COMMERCE. VIOLATIONS OF THESE REGULATIONS ARE PUNISHABLE BY FINE,

IMPRISONMENT, OR BOTH.

REV 03/2024

.1

.02

.005

.25

A A

B B

C C

D D

E E

7.219

E

E

6 2X

20 4X

18 2X

PIN END FLUSH OR SUB

FLUSH WITH OUTER FACE

10 2X

25 2X

9.174

85.5

SECTION E-E

TYP 4 PLACES

20 2X

PIN END FLUSH OR SUB

FLUSH WITH OUTER FACE

TYP 4 PLACES

TOLERANCE (INCH)

C

INTERPRET PER ASME Y14.5-2009

X.X

X.XX

X.XXX

125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

CAGE CODE

APPROX. WEIGHT

231.8

THIRD ANGLE PROJECTION SCALE:

1:5

DO NOT SCALE

FROM DRAWING

N/A

MATERIAL:

NBOC MLV

PROJECT:

N/A

NEXT ASSEMBLY:

STAGE 3 ASSEMBLY, BOOM FAILSAFE,

NBOC MLV

TITLE:

DATE:

DES.

CHK.

DFT.

ENG.

08-20013 REV.

ASHEET 6 OF 7

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED

COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE OBTAINED FROM THE BUREAU OF INDUSTRY AND SECURITY, UNITED STATES

DEPARTMENT OF COMMERCE. VIOLATIONS OF THESE REGULATIONS ARE PUNISHABLE BY FINE,

IMPRISONMENT, OR BOTH.

REV 03/2024

.1

.02

.005

.25

A A

B B

C C

D D

E E

77.5

6.219

F

F

6 2X

20 4X

18 2X

8.174

SECTION F-F

10 2X

25 2X

TYP 4 PLACES

PIN END FLUSH OR SUB

FLUSH WITH OUTER FACE

TOLERANCE (INCH)

C

INTERPRET PER ASME Y14.5-2009

X.X

X.XX

X.XXX

125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

CAGE CODE

APPROX. WEIGHT

186.8

THIRD ANGLE PROJECTION SCALE:

1:5

DO NOT SCALE

FROM DRAWING

N/A

MATERIAL:

NBOC MLV

PROJECT:

N/A

NEXT ASSEMBLY:

STAGE 4 ASSEMBLY, BOOM FAILSAFE,

NBOC MLV

TITLE:

DATE:

DES.

CHK.

DFT.

ENG.

REV.

ASHEET 7 OF 7

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED

COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE OBTAINED FROM THE BUREAU OF INDUSTRY AND SECURITY, UNITED STATES

DEPARTMENT OF COMMERCE. VIOLATIONS OF THESE REGULATIONS ARE PUNISHABLE BY FINE,

IMPRISONMENT, OR BOTH.

REV 03/2024

.1

.02

.005

.25

A A

B B

C C

D D

E E

1.250 1.35 1.50

.5

.0

.600

R.06 .100

.2

.6

2X R.25

2X .433in 11mm THRU 4.

08-20013-01-XX-YY

NOTES (UNLESS OTHERWISE SPECIFIED):

ALL DIMENSIONS IN INCHES UNLESS OTHERWISE SPECIFIED1.

FASTENER CLEARANCE HOLE TOLERANCES PER ASME B18.2.8-19992.

OR ISO 273-1979 FOR SIZES NOT COVERED BY ASME B18.2.8-1999

REMOVE BURRS AND BREAK SHARP EDGES .005-.010 MAX3.

STAMP IN 0.13 HIGH CHARACTERS4.

XX = LOT NUMBER1.

YY = SERIAL NUMBER2.

POST WELD INSPECTION, EXCEPT WHERE NOTED:5.

REMOVE ALL SURFACE RUST, OIL AND GREASE PER NASA-1.

STD-5008B §4.4.2 TO INCLUDE SUB-SECTIONS

ALL SURFACES SHALL BE DEGREASED AND DRY PRIOR TO2.

APPLYING PRIMER

APPLY CARBOLINE CARBOZINC 11 WB PRIMER PER NASA-3.

STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS

APPLY CARBOLINE CARBOACRYLIC 3358 MIDCOAT4.

(BROWN) PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-

SECTIONS

APPLY A MINIMUM OF TWO COATS CARBOLINE5.

CARBOACRYLIC 3359 TOPCOAT (CARBOLINE COLOR CODE

N656, EQUIVALENT FED-STD-595 COLOR YELLOW, NO.

13538) PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-

SECTIONS

DATE REV. DESCRIPTION ENG/DFT

9/13/2024 - ORIGINAL RELEASE KWS

SHEET 1 OF 1

A36

NBOC MLV

08-20013

ENG.

DFT.

CHK.

DES.

WEDGE BLOCK, BOOM FAILSAFE,

NBOC MLV

DO NOT SCALE

FROM DRAWING

THIRD ANGLE PROJECTION

125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

TOLERANCE (INCH)

B

NEXT ASSEMBLY:

PROJECT:

2:1

SCALE:

MATERIAL:

TITLE:

DATE:

REV.08-20013-01

X.X

X.XX

X.XXX

.1

.02

.005

.25

APPROX. WEIGHT

CAGE CODE

0.3

REV 03/2024

INTERPRET PER ASME Y14.5-2009

A A

B B

C C

D D

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT

IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE OBTAINED FROM THE BUREAU OF INDUSTRY AND SECURITY, UNITED STATES DEPARTMENT OF COMMERCE.

VIOLATIONS OF THESE REGULATIONS ARE PUNISHABLE BY FINE, IMPRISONMENT, OR BOTH.

2X M10X1.5 - 6H THRU ALL

1.880 THRU ALL

.750

1.500

4.000

2.000

6X M4X0.7 - 6H THRU ALL

3X .394in±.002 10mm±0.05 THRU ALL

.6

1.

2.

3.

8.

.0

4.

.014 M A B C

.014 A B C

.014 A B C

0.014 A B C

B

C

9X EQ SP @

6.00 = 54.00

10X 1.880 THRU ALL 3X .394in±.002 10mm±0.05 THRU ALL

3X 2.500

3X 1.250

6X M4X0.7 - 6H THRU ALL

1.

TY

P

PL

A

C

ES

7.

.0

.0

4.

08-20013-02-XX-YY

.014 M C B A

.014 C B A

0.014 A B C

A

4X R.75

8X8X.375 STK

5.

NOTES (UNLESS OTHERWISE SPECIFIED):

ALL DIMENSIONS IN INCHES UNLESS OTHERWISE SPECIFIED1.

FASTENER CLEARANCE CLOSE FIT HOLE TOLERANCES PER ASME B18.2.8-1999 OR ISO 273-1979 FOR SIZES NOT COVERED BY ASME2.

B18.2.8-1999

REMOVE BURRS AND BREAK SHARP EDGES .005-.010 MAX3.

STAMP IN 0.13 HIGH CHARACTERS4.

XX = LOT NUMBER1.

YY = SERIAL NUMBER2.

COAT ALL INTERNAL SURFACES WITH MIL-PRF GRADE 4 CLASS 1 CORROSION PROTECTANT PRIOR TO SHIPPING5.

EXCEPT WHERE NOTED:6.

REMOVE ALL SURFACE RUST, OIL AND GREASE PER NASA-STD-5008B §4.4.2 TO INCLUDE SUB-SECTIONS1.

ALL SURFACES SHALL BE DEGREASED AND DRY PRIOR TO APPLYING PRIMER2.

APPLY CARBOLINE CARBOZINC 11 WB PRIMER PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS3.

APPLY CARBOLINE CARBOACRYLIC 3358 MIDCOAT (BROWN) PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS4.

APPLY A MINIMUM OF TWO COATS CARBOLINE CARBOACRYLIC 3359 TOPCOAT (CARBOLINE COLOR CODE C900,5.

EQUIVALENT FED-STD-595 COLOR BLACK, NO. 17038) PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS

DATE REV. DESCRIPTION ENG/DFT

9/13/2024 - ORIGINAL RELEASE KWS

SHEET 1 OF 1

ENG.

DFT.

CHK.

DES.

STAGE 2, BOOM FAILSAFE, NBOC MLV

-125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

C

SCALE:

TITLE:

REV.08-20013-02

257.1

APPROX. WEIGHT

CAGE CODE

.1

.02

.005

.25

X.X

X.XX

X.XXX

TOLERANCE (INCH)

THIRD ANGLE PROJECTION

INTERPRET PER ASME Y14.5-2009

Shaped A500 Gr. C

MATERIAL:

PROJECT:

DO NOT SCALE

FROM DRAWING

NEXT ASSEMBLY:

08-20013

NBOC MLV

1:5

REV 03/2024

DATE:A A

B B

C C

D D

E E

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED

COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE OBTAINED FROM THE BUREAU OF INDUSTRY AND SECURITY, UNITED STATES

DEPARTMENT OF COMMERCE. VIOLATIONS OF THESE REGULATIONS ARE PUNISHABLE BY FINE,

IMPRISONMENT, OR BOTH.

12 EQ SP @

6.00 = 72.00

13X 1.880 THRU ALL

2.500

1.250 3X .394in±.002 10mm±0.05 THRU ALL

6X M4X0.7 - 6H THRU ALL

7.0

1.

5.

.0

.0

5.

.014 M A B C .014 M A B C

.014 M A B C

B C

66.50 2.500

1.250

2X 1.880 THRU ALL

3X .394in±.002 10mm±0.05 THRU ALL

6X M4X0.7 - 6H THRU ALL

7.0

1.

.0

.0

2.

4.

08-20013-03-XX-YY.014 M C B A

.014 M C B A

.014 M C B A

A

7 X 7 X .375 TUBE STK

5.

NOTES (UNLESS OTHERWISE SPECIFIED):

ALL DIMENSIONS IN INCHES UNLESS OTHERWISE SPECIFIED1.

FASTENER CLEARANCE CLOSE FIT HOLE TOLERANCES PER ASME B18.2.8-1999 OR ISO 273-1979 FOR SIZES NOT COVERED BY2.

ASME B18.2.8-1999

REMOVE BURRS AND BREAK SHARP EDGES .005-.010 MAX3.

STAMP IN 0.13 HIGH CHARACTERS4.

XX = LOT NUMBER1.

YY = SERIAL NUMBER2.

COAT ALL INTERNAL SURFACES WITH MIL-PRF GRADE 4 CLASS 1 CORROSION PROTECTANT PRIOR TO SHIPPING5.

EXCEPT WHERE NOTED:6.

REMOVE ALL SURFACE RUST, OIL AND GREASE PER NASA-STD-5008B §4.4.2 TO INCLUDE SUB-SECTIONS1.

ALL SURFACES SHALL BE DEGREASED AND DRY PRIOR TO APPLYING PRIMER2.

APPLY CARBOLINE CARBOZINC 11 WB PRIMER PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS3.

APPLY CARBOLINE CARBOACRYLIC 3358 MIDCOAT (BROWN) PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS4.

APPLY A MINIMUM OF TWO COATS CARBOLINE CARBOACRYLIC 3359 TOPCOAT (CARBOLINE COLOR CODE C900,5.

EQUIVALENT FED-STD-595 COLOR BLACK, NO. 17038) PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS

DATE REV. DESCRIPTION ENG/DFT

9/13/2024 - ORIGINAL RELEASE MTT

SHEET 1 OF 1

ENG.

DFT.

CHK.

DES.

STAGE 3, BOOM FAILSAFE, NBOC MLV

-125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

C

SCALE:

TITLE:

REV.08-20013-03

223.1

APPROX. WEIGHT

CAGE CODE

.1

.02

.005

.25

X.X

X.XX

X.XXX

TOLERANCE (INCH)

THIRD ANGLE PROJECTION

INTERPRET PER ASME Y14.5-2009

SHAPED A500 GR. C

MATERIAL:

PROJECT:

DO NOT SCALE

FROM DRAWING

NEXT ASSEMBLY:

08-20013

NBOC_MLV

1:10

REV 03/2024

DATE:A A

B B

C C

D D

E E

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED

COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE OBTAINED FROM THE BUREAU OF INDUSTRY AND SECURITY, UNITED STATES

2X .177in 4.50mm THRU ALL .354in 9mm X 90°

.394in±.002 10mm±0.05 THRU ALL

2.50

1.250

.750

12 GAUGE STK

1.50

4.00

4X R.25 4.

08-20013-04-XX-YY

NOTES (UNLESS OTHERWISE SPECIFIED):

ALL DIMENSIONS IN INCHES UNLESS OTHERWISE SPECIFIED1.

FASTENER CLEARANCE HOLE TOLERANCES PER ASME B18.2.8-1999 2.

OR ISO 273-1979 FOR SIZES NOT COVERED BY ASME B18.2.8-1999

REMOVE BURRS AND BREAK SHARP EDGES .005-.010 MAX3.

STAMP IN 0.13 HIGH CHARACTERS4.

XX = LOT NUMBER1.

YY = SERIAL NUMBER2.

DATE REV. DESCRIPTION ENG/DFT

9/20/2024 - ORIGINAL RELEASE KWS

SHEET 1 OF 1

316 SS

NBOC MLV

08-20013

ENG.

DFT.

CHK.

DES.

INTERNAL SLIDE, BOOM FAILSAFE,

NBOC MLV

DO NOT SCALE

FROM DRAWING

THIRD ANGLE PROJECTION

125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

TOLERANCE (INCH)

B

NEXT ASSEMBLY:

PROJECT:

1:1

SCALE:

MATERIAL:

TITLE:

DATE:

REV.08-20013-04

X.X

X.XX

X.XXX

.1

.02

.005

.25

APPROX. WEIGHT

CAGE CODE

0.2

REV 03/2024

INTERPRET PER ASME Y14.5-2009

A A

B B

C C

D D

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT

IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE

1.850

.26in 6.60mm THRU ALL .43in 11mm 1.34in 33.94mm

A

A

R.03

R.03

.06 X .06

50.63°

1.11

1.695

SECTION A-A

5.

08-20013-05-XX-YY

NOTES (UNLESS OTHERWISE SPECIFIED):

ALL DIMENSIONS IN INCHES UNLESS OTHERWISE SPECIFIED1.

FASTENER CLEARANCE HOLE TOLERANCES PER ASME B18.2.8-19992.

OR ISO 273-1979 FOR SIZES NOT COVERED BY ASME B18.2.8-1999

REMOVE BURRS AND BREAK SHARP EDGES .005-.010 MAX3.

POST MACHINING, COAT PART WITH MIL-PRF-16173E GRADE 44.

CLASS 1 PRIOR TO SHIPPING

STAMP IN 0.13 HIGH CHARACTERS5.

XX = LOT NUMBER1.

YY = SERIAL NUMBER2.

DATE REV. DESCRIPTION ENG/DFT

9/20/2024 - ORIGINAL RELEASE KWS

SHEET 1 OF 1

AISI 1045

NBOC MLV

08-20013

ENG.

DFT.

CHK.

DES.

TAPERED PIN, BOOM FAILSAFE, NBOC

MLV

DO NOT SCALE

FROM DRAWING

THIRD ANGLE PROJECTION

125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

TOLERANCE (INCH)

B

NEXT ASSEMBLY:

PROJECT:

1:1

SCALE:

MATERIAL:

TITLE:

DATE:

REV.08-20013-05

X.X

X.XX

X.XXX

.1

.02

.005

.25

APPROX. WEIGHT

CAGE CODE

1.0

REV 03/2024

INTERPRET PER ASME Y14.5-2009

A A

B B

C C

D D

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT

IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE

7.

08-20013-100-XX-YY

4 2X

2 4X

BACKGOUGE

.125

TYP 2 PLACES

.125

TYP 4 PLACES

82.5

.3+ .06 .00

.6+ .06 .03

3.25

3.

TUBE AND WELD

SHOULD NOT PROTRUDE PAST

PLATE MATING SURFACE

GRIND FLAT IF NEEDED

BOTH SIDES OF TUBE

.1 A

A

B

NOTES (UNLESS OTHERWISE SPECIFIED):

ALL DIMENSIONS IN INCHES UNLESS OTHERWISE1.

SPECIFIED

FASTENER CLEARANCE HOLE TOLERANCES PER2.

ASME B18.2.8-1999 OR ISO 273-1979 FOR SIZES

NOT COVERED BY ASME B18.2.8-1999

REMOVE BURRS AND BREAK SHARP EDGES .005-3.

.010 MAX

PRE-WELD MACHINING DIMENSIONS ON SHEET 2.4.

EACH COMPONENT SHALL BE TAGGED WITH P/N,

L/N, AND S/N UNTIL THE COMPONENTS ARE

WELDED TO FORM WELDMENT P/N OF THIS

DOCUMENT

ALL WELDING AND INSPECTION SHALL BE IN5.

ACCORDANCE WITH AWS D1.1/D1.1M:2020

FILLER METAL1.

ER70S-6 AWS A5.181.

ER70S-3 AWS A5.182.

E7018-1 AWS A5.13.

ALL WELDS SHALL BE INSPECTED VISUALLY AND6.

INSPECTED BY EITHER MAGNETIC PARTICLE

TESTING (MT) OR LIQUID PENETRANT TESTING (PT)

STAMP IN 0.375 HIGH CHARACTERS7.

XX = LOT NUMBER1.

YY = SERIAL NUMBER2.

POST WELD INSPECTION, EXCEPT WHERE NOTED:8.

REMOVE ALL SURFACE RUST, OIL AND1.

GREASE PER NASA-STD-5008B §4.4.2 TO

INCLUDE SUB-SECTIONS

ALL SURFACES SHALL BE DEGREASED AND2.

DRY PRIOR TO APPLYING PRIMER

APPLY CARBOLINE CARBOZINC 11 WB3.

PRIMER PER NASA-STD-5008B §4.4.3 TO

INCLUDE SUB-SECTIONS

APPLY CARBOLINE CARBOACRYLIC 33584.

MIDCOAT (BROWN) PER NASA-STD-5008B

§4.4.3 TO INCLUDE SUB-SECTIONS

APPLY A MINIMUM OF TWO COATS5.

CARBOLINE CARBOACRYLIC 3359 TOPCOAT

(CARBOLINE COLOR CODE C900,

EQUIVALENT FED-STD-595 COLOR BLACK,

NO. 17038) PER NASA-STD-5008B §4.4.3 TO

INCLUDE SUB-SECTIONS

DATE REV. DESCRIPTION ENG/DFT

9/20/2024 - ORIGINAL RELEASE KWS

ITEM

NO. QTY. PART NO. DESCRIPTION LENGTH MATERIAL SOURCE SOURCE

PART NO. WEIGHT

1 1 08-20013-101 BOTTOM FLANGE, 1.0 STK, BOOM

FAILSAFE, NBOC MLV A572 GR. 50 5.9

2 4 08-20013-102 CYLINDER TAB, 0.25 STK, BOOM

FAILSAFE, NBOC MLV A572 GR. 50 0.2

3 1 08-20013-103 TS9X9X0.375 82.5 SHAPED

A500 GR. C 293.4

4 2 08-20013-104 SENSOR TAB, 0.25 STK, BOOM FAILSAFE,

NBOC MLV A572 GR. 50 0.7

SHEET 1 OF 2

ENG.

DFT.

CHK.

DES.

STAGE 1, BOOM FAILSAFE, NBOC MLV

-125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

C

SCALE:

TITLE:

REV.08-20013-100

301.6

APPROX. WEIGHT

CAGE CODE

.1

.02

.005

.25

X.X

X.XX

X.XXX

TOLERANCE (INCH)

THIRD ANGLE PROJECTION

INTERPRET PER ASME Y14.5-2009

SHAPED A500 GR. C

MATERIAL:

PROJECT:

DO NOT SCALE

FROM DRAWING

NEXT ASSEMBLY:

08-20013

NBOC MLV

1:10

REV 03/2024

DATE:A A

B B

C C

D D

E E

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED

COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE OBTAINED FROM THE BUREAU OF INDUSTRY AND SECURITY, UNITED STATES

9.0+ .06 .00

9.0+ .06 .00

11.50

11.50

1.25

1.25

12X .433in 11mm THRU ALL

3.175

.600

10.300

10.300

2 EQ SP@

2.275 = 5.150

2 EQ SP@

2.275 = 5.150

3.175

.600

.014 M B C D

CD

.650 THRU

4.00

.75

R.65

23.5°

.394in±.002 10mm±0.05 THRU ALL

2X M4X0.7 - 6H THRU ALL

2.500

1.250

2.750

1.375 2.750

4X M10X1.5 - 6H THRU ALL

1.880 THRU ALL

9.0 STK

.1

2.

9.0 STK

.750 1.500

2.500

5.000

1.250

2.500

2X M10X1.5 - 6H THRU ALL

4X M4X0.7 - 6H THRU ALL

2X .394in±.002 10mm±0.05 THRU ALL 0

8X M4X0.7 - 6H THRU ALL

.3

.338

1.519

2.069

3.250 3.50

PN: 08-20013-101

0.5 STK

SCALE 1:4

PN: 08-20013-102

0.25 STK

SCALE 1:1

PN: 08-20013-103

SCALE 1:4

PN: 08-20013-104

0.25 STK

SCALE 1:1

4.

SHEET 2 OF 2

ENG.

DFT.

CHK.

DES.

MACHINED DIMENSIONS FOR STAGE

1, BOOM FAILSAFE, NBOC MLV

-125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

C

SCALE:

TITLE:

REV.08-20013-100

SEE CUTLIST

APPROX. WEIGHT

CAGE CODE

.1

.02

.005

.25

X.X

X.XX

X.XXX

TOLERANCE (INCH)

THIRD ANGLE PROJECTION

INTERPRET PER ASME Y14.5-2009

SHAPED A500 GR. C

MATERIAL:

PROJECT:

DO NOT SCALE

FROM DRAWING

NEXT ASSEMBLY:

N/A

NBOC MLV

1:12

REV 03/2024

DATE:A A

B B

C C

D D

E E

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED

COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE OBTAINED FROM THE BUREAU OF INDUSTRY AND SECURITY, UNITED STATES

DEPARTMENT OF COMMERCE. VIOLATIONS OF THESE REGULATIONS ARE PUNISHABLE BY FINE,

By Christopher Leikam at 9:53 am, Sep 25, 2024

1.880

1.0 STK

71.5

6.00

2.00

3.00

26.50

A

6.

08-20013-200-XX-YY

A

A

0.02 B A C

A

BACKGOUGE

1.800

5.00 6.00

21.50

1.880 THRU ALL

7 EQ SP @

6.00 = 42.00

2.50

3.00

2.50

B

FULL R

0.02 A B C

0.02 A B C

C

B

ISOMETRIC VIEW

FOR REFERENCE ONLY

SCALE: 1:8

13.000

2X 1.250

2X .394±.002 10.00±0.05 THRU ALL

4X M4X0.7 - 6H THRU ALL

2X 2.500

3.00 4.00

DETAIL A

SCALE 1 : 4

.014 M B A C .014 M B A C

4X R.75

4X M4X0.7 - 6H THRU ALL

2X 1.250

2X 2.500

13.000

2X .394±.002 10.00±0.05 THRU ALL

3.000

4.00

DETAIL B

SCALE 1 : 4

.014 M A B C

.014 M A B C

NOTES (UNLESS OTHERWISE SPECIFIED):

ALL DIMENSIONS IN INCHES UNLESS OTHERWISE SPECIFIED1.

FASTENER CLEARANCE HOLE TOLERANCES PER ASME B18.2.8-1999 OR ISO 273-1979 FOR SIZES NOT COVERED BY ASME B18.2.8-19992.

REMOVE BURRS AND BREAK SHARP EDGES .005-.010 MAX3.

ALL WELDING AND INSPECTION SHALL BE IN ACCORDANCE WITH AWS D1.1/D1.1M:20204.

FILLER METAL1.

ER70S-6 AWS A5.181.

ER70S-3 AWS A5.182.

E7018-1 AWS A5.13.

ALL WELDS SHALL BE INSPECTED VISUALLY AND INSPECTED BY EITHER MAGNETIC PARTICLE TESTING (MT) OR LIQUID PENETRANT TESTING (PT)5.

STAMP IN 0.13 HIGH CHARACTERS6.

XX = LOT NUMBER1.

YY = SERIAL NUMBER2.

POST WELD INSPECTION, EXCEPT WHERE NOTED:7.

REMOVE ALL SURFACE RUST, OIL AND GREASE PER NASA-STD-5008B §4.4.2 TO INCLUDE SUB-SECTIONS1.

ALL SURFACES SHALL BE DEGREASED AND DRY PRIOR TO APPLYING PRIMER2.

APPLY CARBOLINE CARBOZINC 11 WB PRIMER PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS3.

APPLY CARBOLINE CARBOACRYLIC 3358 MIDCOAT (BROWN) PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS4.

APPLY A MINIMUM OF TWO COATS CARBOLINE CARBOACRYLIC 3359 TOPCOAT (CARBOLINE COLOR CODE C900, EQUIVALENT FED-STD-595 COLOR BLACK, NO. 17038)5.

PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS

A

DATE REV. DESCRIPTION ENG/DFT

9/19/2024 - ORIGINAL RELEASE MTT

10/16/2024 A INCREASED CAP TO 1.0 THICKNESS AND DECREASED TUBE

LENGTH TO ACCOUNT FOR EXTRA LENGTH PER CR 2750 KWS

ITEM

NO. QTY. PART NO. DESCRIPTION LENGTH MATERIAL SOURCE SOURCE

PART NO. WEIGHT

1 1 08-20013-201 TUBE CAP, 1.0 STK, BOOM FAILSAFE,

NBOC MLV A572 GR. 50 9.94

2 1 08-20013-202 PAD EYE, 2.0 STK, BOOM FAILSAFE,

NBOC MLV A572 GR. 50 11.07

3 1 08-20013-203 TS6X6X0.375 71.5 SHAPED

A500 GR. C 158.31

SHEET 1 OF 1

A572 Gr. 50

NBOC MLV

08-20013

ENG.

DFT.

CHK.

DES.

STAGE 4, BOOM FAILSAFE, NBOC MLV

A

DO NOT SCALE

FROM DRAWING

THIRD ANGLE PROJECTION

125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

TOLERANCE (INCH)

D

NEXT ASSEMBLY:

PROJECT:

1:8

SCALE:

INTERPRET PER ASME Y14.5-2009

MATERIAL:

TITLE:

DATE:

REV.08-20013-200

X.X

X.XX

X.XXX

.1

.02

.005

.25

APPROX. WEIGHT

CAGE CODE

179.32

REV 03/2024

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT- CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE OBTAINED FROM THE BUREAU OF INDUSTRY AND SECURITY, UNITED STATES DEPARTMENT OF COMMERCE. VIOLATIONS OF THESE REGULATIONS ARE PUNISHABLE BY FINE, IMPRISONMENT, OR BOTH.

A A

B B

C C

D D

E E

F F

M6x1.0-6H THRU ALL

AA

0.014 A B

B

B

1/4

.20

1.20

2.82

2X R.03

.03 X 45°.03 X 45°

.03 X 45°

.03 X 45°

R.03

1.870

2.52

.38 .25 .70

SECTION A-A

0.02 A B

0.02 A B

0.02 A B

B

A

B

6.

08-20013-300-XX-YY

.03 X 45°

OUTER OF ITEM 2

2.50

2.12

SECTION B-B

NOTES (UNLESS OTHERWISE SPECIFIED):

ALL DIMENSIONS IN INCHES UNLESS OTHERWISE SPECIFIED1.

FASTENER CLEARANCE HOLE TOLERANCES PER ASME B18.2.8-1999 OR ISO 273-1979 FOR SIZES NOT COVERED BY ASME B18.2.8-19992.

REMOVE BURRS AND BREAK SHARP EDGES .005-.010 MAX3.

ALL WELDING AND INSPECTION SHALL BE IN ACCORDANCE WITH AWS D1.1/D1.1M:20204.

FILLER METAL1.

ER70S-6 AWS A5.181.

ER70S-3 AWS A5.182.

E7018-1 AWS A5.13.

ALL WELDS SHALL BE INSPECTED VISUALLY AND INSPECTED BY EITHER MAGNETIC PARTICLE TESTING (MT) OR LIQUID PENETRANT TESTING (PT)5.

STAMP IN 0.13 HIGH CHARACTERS6.

XX = LOT NUMBER1.

YY = SERIAL NUMBER2.

POST WELD INSPECTION, EXCEPT WHERE NOTED:7.

REMOVE ALL SURFACE RUST, OIL AND GREASE PER NASA-STD-5008B §4.4.2 TO INCLUDE SUB-SECTIONS1.

ALL SURFACES SHALL BE DEGREASED AND DRY PRIOR TO APPLYING PRIMER2.

APPLY CARBOLINE CARBOZINC 11 WB PRIMER PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS3.

APPLY CARBOLINE CARBOACRYLIC 3358 MIDCOAT (BROWN) PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS4.

APPLY A MINIMUM OF TWO COATS CARBOLINE CARBOACRYLIC 3359 TOPCOAT (CARBOLINE COLOR CODE C900, EQUIVALENT FED-5.

STD-595 COLOR BLACK, NO. 17038) PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS

DATE REV. DESCRIPTION ENG/DFT

9/20/2024 - ORIGINAL RELEASE KWS

ITEM

NO. QTY. PART NO. DESCRIPTION LENGTH MATERIAL SOURCE SOURCE

PART NO. WEIGHT

1 1 08-20013-301 SPRING PERCH, SPRING PIN PLUNGER,

BOOM FAILSAFE, NBOC MLV A572 GR. 50 0.56

2 1 08-20013-302 TUBE 2.5 OD X 0.188 WALL 2.50 DOM A513

GR. 1010 0.98

SHEET 1 OF 1

ENG.

DFT.

CHK.

DES.

SPRING PIN PLUNGER, BOOM

FAILSAFE, NBOC MLV

-125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

C

SCALE:

TITLE:

REV.

1.54

APPROX. WEIGHT

CAGE CODE

.1

.02

.005

.25

X.X

X.XX

X.XXX

TOLERANCE (INCH)

THIRD ANGLE PROJECTION

INTERPRET PER ASME Y14.5-2009

SEE CUTLIST

MATERIAL:

PROJECT:

DO NOT SCALE

FROM DRAWING

NEXT ASSEMBLY:

08-20013

NBOC MLV

1:1

REV 03/2024

DATE:A A

B B

C C

D D

E E

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED

COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE OBTAINED FROM THE BUREAU OF INDUSTRY AND SECURITY, UNITED STATES

DEPARTMENT OF COMMERCE. VIOLATIONS OF THESE REGULATIONS ARE PUNISHABLE BY FINE,

08-20013-300

B

B

1/4

2.56 3.00

.03 X 45°

OUTER DIAMETER OF ITEM 2

SECTION B-B

M6x1.0-6H THRU ALL

AA

0.014 A B

.38

1.870

1.20

.70

.20

3.020

3.52

.25

.03 X 45°

.03 X 45° .03 X 45°

.03 X 45°

R.03

2X R.03

SECTION A-A

SCALE 1 : 1

0.02 A B

0.02 A B

0.02 A B

B

A 6.

08-20013-400-XX-YY

NOTES (UNLESS OTHERWISE SPECIFIED):

ALL DIMENSIONS IN INCHES UNLESS OTHERWISE SPECIFIED1.

FASTENER CLEARANCE HOLE TOLERANCES PER ASME B18.2.8-1999 OR ISO 273-1979 FOR SIZES NOT COVERED BY ASME B18.2.8-19992.

REMOVE BURRS AND BREAK SHARP EDGES .005-.010 MAX3.

ALL WELDING AND INSPECTION SHALL BE IN ACCORDANCE WITH AWS D1.1/D1.1M:20204.

FILLER METAL1.

ER70S-6 AWS A5.181.

ER70S-3 AWS A5.182.

E7018-1 AWS A5.13.

ALL WELDS SHALL BE INSPECTED VISUALLY AND INSPECTED BY EITHER MAGNETIC PARTICLE TESTING (MT) OR LIQUID PENETRANT TESTING (PT)5.

STAMP IN 0.13 HIGH CHARACTERS6.

XX = LOT NUMBER1.

YY = SERIAL NUMBER2.

POST WELD INSPECTION, EXCEPT WHERE NOTED:7.

REMOVE ALL SURFACE RUST, OIL AND GREASE PER NASA-STD-5008B §4.4.2 TO INCLUDE SUB-SECTIONS1.

ALL SURFACES SHALL BE DEGREASED AND DRY PRIOR TO APPLYING PRIMER2.

APPLY CARBOLINE CARBOZINC 11 WB PRIMER PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS3.

APPLY CARBOLINE CARBOACRYLIC 3358 MIDCOAT (BROWN) PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS4.

APPLY A MINIMUM OF TWO COATS CARBOLINE CARBOACRYLIC 3359 TOPCOAT (CARBOLINE COLOR CODE C900, EQUIVALENT FED-5.

STD-595 COLOR BLACK, NO. 17038) PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS

ITEM

NO. QTY. PART NO. DESCRIPTION LENGTH MATERIAL SOURCE SOURCE

PART NO. WEIGHT

1 1 08-20013-401

LOWER BODY SPRING PERCH, LOWER

SPRING PIN BODY, BOOM FAILSAFE,

NBOC MLV

A572 GR. 50 0.93

2 1 08-20013-402 TUBE 3 OD X 0.219 WALL 3.38 DOM A513

GR. 1010 1.84

DATE REV. DESCRIPTION ENG/DFT

9/20/2024 - ORIGINAL RELEASE KWS

SHEET 1 OF 1

ENG.

DFT.

CHK.

DES.

LOWER SPING PIN BODY, BOOM

FAILSAFE, NBOC MLV

-125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

C

SCALE:

TITLE:

REV.08-20013-400

2.77

APPROX. WEIGHT

CAGE CODE

.1

.01

.005

.25

X.X

X.XX

X.XXX

TOLERANCE (INCH)

THIRD ANGLE PROJECTION

INTERPRET PER ASME Y14.5-2009

SEE CUTLIST

MATERIAL:

PROJECT:

DO NOT SCALE

FROM DRAWING

NEXT ASSEMBLY:

08-20013

NBOC MLV

1:1

DATE: A

B B

C C

D D

E E

6 5

REV 03/2024

A

6 5

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED

COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE OBTAINED FROM THE BUREAU OF INDUSTRY AND SECURITY, UNITED STATES

11.50 2X 2.580

10.320

2X 2.580

10.320

4X R3.00

11.50

.433 11.00 THRU ALL

6.

08-20013-500-XX-YY

0.014 A B C

B C

1.00 STK

2.00 STK

.010

0.01 A C

BACKGOUGE

7.00

1.800±.003

5.50

2.25

2X 11°

3.500

0.02 C A B

0.02 C A B

A

NOTES (UNLESS OTHERWISE SPECIFIED):

ALL DIMENSIONS IN INCHES UNLESS OTHERWISE SPECIFIED1.

FASTENER CLEARANCE CLOSE FIT HOLE TOLERANCES PER ASME B18.2.8-1999 OR ISO 273-1979 FOR2.

SIZES NOT COVERED BY ASME B18.2.8-1999

REMOVE BURRS AND BREAK SHARP EDGES .005-.010 MAX3.

ALL WELDING AND INSPECTION SHALL BE IN ACCORDANCE WITH AWS D1.1/D1.1M:20204.

FILLER METAL1.

ER70S-6 AWS A5.181.

ER70S-3 AWS A5.182.

E7018-1 AWS A5.13.

ALL WELDS SHALL BE INSPECTED VISUALLY AND INSPECTED BY EITHER MAGNETIC PARTICLE TESTING5.

(MT) OR LIQUID PENETRANT TESTING (PT)

STAMP IN 0.13 HIGH CHARACTERS6.

XX = LOT NUMBER1.

YY = SERIAL NUMBER2.

POST WELD INSPECTION, EXCEPT WHERE NOTED:7.

REMOVE ALL SURFACE RUST, OIL AND GREASE PER NASA-STD-5008B §4.4.2 TO INCLUDE1.

SUB-SECTIONS

ALL SURFACES SHALL BE DEGREASED AND DRY PRIOR TO APPLYING PRIMER2.

APPLY CARBOLINE CARBOZINC 11 WB PRIMER PER NASA-STD-5008B §4.4.3 TO INCLUDE3.

SUB-SECTIONS

APPLY CARBOLINE CARBOACRYLIC 3358 MIDCOAT (BROWN) PER NASA-STD-5008B §4.4.34.

TO INCLUDE SUB-SECTIONS

APPLY A MINIMUM OF TWO COATS CARBOLINE CARBOACRYLIC 3359 TOPCOAT5.

(CARBOLINE COLOR CODE C900, EQUIVALENT FED-STD-595 COLOR BLACK, NO. 17038)

PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS

A

A

DATE REV DESCRIPTION ENG/DRAFT

9/13/2024 - ORIGINAL RELEASE KS/MT

10/16/2024 A

INCREASED BASE THICKNESS TO 1.0 STK AND

DECREASED HOLE LOCATION IN PAD EYE FROM 4.0 TO

3.5 TO ACCOUNT PER CR 2751

KWS

ITEM

NO. QTY. PART NO. DESCRIPTION LENGTH MATERIAL SOURCE SOURCE

PART NO. WEIGHT

1 1 08-20013-501 PAD EYE, 2.0 STK, FOOT, BOOM

FAILSAFE, NBOC MLV A572 GR. 50 17.59

2 1 08-20013-502 BASE, 1.0 STK, FOOT, BOOM FAILSAFE,

NBOC MLV A572 GR. 50 34.37

SHEET 1 OF 1

ENG.

DFT.

CHK.

DES.

FOOT, BOOM FAILSAFE, NBOC MLV

A125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

C

SCALE:

TITLE:

REV.08-20013-500

51.97

APPROX. WEIGHT

CAGE CODE

.1

.02

.005

.25

X.X

X.XX

X.XXX

TOLERANCE (INCH)

THIRD ANGLE PROJECTION

INTERPRET PER ASME Y14.5-2009

A572 Gr. 50

MATERIAL:

PROJECT:

DO NOT SCALE

FROM DRAWING

NEXT ASSEMBLY:

08-20013

NBOC MLV

1:4

REV 03/2024

DATE:A A

B B

C C

D D

E E

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED

COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE OBTAINED FROM THE BUREAU OF INDUSTRY AND SECURITY, UNITED STATES

1/4

2.56

3.00

.03 X 45°

OUTER DIAMETER OF ITEM 2

SECTION A-A

M6x1.0 - 6H THRU ALL

BB

0.014 A B

3.020

.20

.25

.38 .70

3.72

1.20

1.87

.03 X 45°

.03 X 45°

.03 X 45°

.03 X 45°

2X R.03

R.03

SECTION B-B

0.02 A B

0.02 A B

0.02 A B

B

A

6.

08-20013-600-XX-YY

NOTES (UNLESS OTHERWISE SPECIFIED):

ALL DIMENSIONS IN INCHES UNLESS OTHERWISE SPECIFIED1.

FASTENER CLEARANCE HOLE TOLERANCES PER ASME B18.2.8-1999 OR ISO 273-1979 FOR SIZES NOT COVERED BY ASME2.

B18.2.8-1999

REMOVE BURRS AND BREAK SHARP EDGES .005-.010 MAX3.

ALL WELDING AND INSPECTION SHALL BE IN ACCORDANCE WITH AWS D1.1/D1.1M:20204.

FILLER METAL1.

ER70S-6 AWS A5.181.

ER70S-3 AWS A5.182.

E7018-1 AWS A5.13.

ALL WELDS SHALL BE INSPECTED VISUALLY AND INSPECTED BY EITHER MAGNETIC PARTICLE TESTING (MT) OR LIQUID5.

PENETRANT TESTING (PT)

STAMP IN 0.13 HIGH CHARACTERS6.

XX = LOT NUMBER1.

YY = SERIAL NUMBER2.

POST WELD INSPECTION, EXCEPT WHERE NOTED:7.

REMOVE ALL SURFACE RUST, OIL AND GREASE PER NASA-STD-5008B §4.4.2 TO INCLUDE SUB-SECTIONS1.

ALL SURFACES SHALL BE DEGREASED AND DRY PRIOR TO APPLYING PRIMER2.

APPLY CARBOLINE CARBOZINC 11 WB PRIMER PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS3.

APPLY CARBOLINE CARBOACRYLIC 3358 MIDCOAT (BROWN) PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-4.

SECTIONS

APPLY A MINIMUM OF TWO COATS CARBOLINE CARBOACRYLIC 3359 TOPCOAT (CARBOLINE COLOR CODE C900,5.

EQUIVALENT FED-STD-595 COLOR BLACK, NO. 17038) PER NASA-STD-5008B §4.4.3 TO INCLUDE SUB-SECTIONS

DATE REV. DESCRIPTION ENG/DFT

9/20/2024 - ORIGINAL RELEASE MTT

ITEM

NO. QTY. PART NO. DESCRIPTION LENGTH MATERIAL SOURCE SOURCE

PART NO. WEIGHT

1 1 08-20013-601

UPPER BODY SPRING PERCH, UPPER

SPRING PIN BODY, BOOM FAILSAFE,

NBOC MLV

A572 GR. 50 1.08

2 1 08-20013-602 TUBE 3 OD X 0.219 WALL 2.38 DOM A513

GR. 1010 1.30

SHEET 1 OF 1

ENG.

DFT.

CHK.

DES.

UPPER SPRING PIN BODY, BOOM

FAILSAFE, NBOC MLV -125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

C

SCALE:

TITLE:

REV.08-20013-600

2.37

APPROX. WEIGHT

CAGE CODE

.1

.02

.005

.25

X.X

X.XX

X.XXX

TOLERANCE (INCH)

THIRD ANGLE PROJECTION

INTERPRET PER ASME Y14.5-2009

SEE CUTLIST

MATERIAL:

PROJECT:

DO NOT SCALE

FROM DRAWING

NEXT ASSEMBLY:

08-20013

NBOC MLV

1:1

REV 03/2024

DATE:

THIS DRAWING IS THE PROPERTY OF THE NASA BALLOON PROGRAM AND MAY NOT BE USED, COPIED, OR DISTRIBUTED (OUTSIDE OF AUTHORIZED CONTRACTORS) FOR ANY PURPOSE OTHER THAN THAT FOR WHICH IT IS SUPPLIED WITHOUT THE EXPRESS WRITTEN AUTHORITY OF THE NASA BALLON PROGRAM.

THIS DOCUMENT CONTAINS INFORMATION WITHIN THE PURVIEW OF THE EXPORT ADMINISTRATION REGULATIONS (EAR), 15 CFR §730-774, AND IS EXPORT-CONTROLLED. IT IS PROHIBITED FOR SALE, EXPORT, RE-EXPORT OR TRANSFER TO ORGANIZATIONS AND NATIONALS OF EMBARGOED

COUNTRIES: CUBA, SUDAN, NORTH KOREA, IRAN, SYRIA AND CRIMEA A REGION OF UKRAINE, UNLESS AN EXPORT LICENSE OBTAINED FROM THE BUREAU OF INDUSTRY AND SECURITY, UNITED STATES

DEPARTMENT OF COMMERCE. VIOLATIONS OF THESE REGULATIONS ARE PUNISHABLE BY FINE,

IMPRISONMENT, OR BOTH.

A A

B B

C C

D D

E E

08-20013 Boom Failsafe
08-20013-01 Wedge Block
08-20013-02 Stage 2, Boom Failsafe
08-20013-03 Stage 3, Boom Failsafe
08-20013-04 Internal Slide
08-20013-05 Tapered Pin
08-20013-100 Stage 1, Boom Failsafe
08-20013-200 Stage 4, Boom Failsafe
08-20013-300 Spring Pin Plunger
08-20013-400 Lower Spring Pin Body
08-20013-500 Foot
08-20013-600 Upper Spring Pin Body

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