08-20007-200_CRADLE AXLE CART NBOC MLV.pdf

A

A

4 2X

8.

08-20007-200-XX-YY

TORQUE HAND TIGHT

SECTION A-A

TYP 2 PLACES

7 2X

12 4X

11 4X

NOTES (UNLESS OTHERWISE SPECIFIED):

ALL DIMENSIONS IN INCHES UNLESS OTHERWISE 1.

SPECIFIED

FASTENER CLEARANCE HOLE TOLERANCES PER ASME 2.

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-.010 3.

MAX.

APPLY MIL-PRF-907H TYPE II GRAPHITE/ALUMINUM 4.

ANTI-SEIZE COMPOUND LIBERALLY TO THREAD OF ALL

FASTENERS AND TORQUE ALL FASTENERS PER TORQUE

TABLE UNLESS OTHERWISE SPECIFIED.

PRE-WELD MACHINING DIMENSIONS ON SH 3. EACH 5.

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, INSPECTION, AND ACCEPTANCE 6.

SHALL BE IN ACCORDANCE WITH AWS

D1.1/D1.1M:2020

FILLER METAL 1.

ER70S-6 AWS A5.181.

ER70S-3 AWS A5.182.

E7018-1 AWS A5.13.

ALL WELDS SHALL BE INSPECTED VISUALLY AND 7.

INSPECTED BY EITHER MAGNETIC PARTICLE TESTING

(MT) OR LIQUID PENETRANT TESTING (PT)

STAMP IN 0.13 HIGH CHARACTERS8.

XX = LOT NUMBER1.

YY = SERIAL NUMBER2.

PAINT ITEM 5 IAW NOTE 9 PRIOR TO ASSEMBLY.9.

AFTER WELDING, COAT ALL INTERNAL SURFACES OF 10.

SQ 4.00 X 4.00 X .25 WALL TUBES WITH MIL-PRF-16173E

GRADE 3 CLASS 1 CORROSION PROTECTANT PRIOR

TO SHIPPING.

POST WELD INSPECTION OF THE COMPONENTS ON 11.

SH2, EXCEPT WHERE NOTED:

REMOVE ALL SURFACE RUST, OIL AND GREASE 1.

PER NASA-STD-5008B §4.4.2 TO INCLUDE SUB-

SECTIONS

ALL SURFACES SHALL BE DEGREASED AND DRY 2.

PRIOR TO APPLYING PRIMER

APPLY CARBOLINE CARBOZINC 11 WB PRIMER 3.

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

SECTIONS

APPLY CARBOLINE CARBOACRYLIC 3358 4.

MIDCOAT (BROWN) PER NASA-STD-5008B §4.4.3

TO INCLUDE SUB-SECTIONS

APPLY A MINIMUM OF TWO COATS CARBOLINE 5.

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

4.

DATE REV. DESCRIPTION ENG/DFT

9/17/2024 - ORIGINAL RELEASE JB

ITEM

NO. QTY PART NO. DESCRIPTION MATERIAL SOURCE SOURCE

PART NO. WEIGHT

1 2 08-20007-202 PLATE, UPRIGHT INTERFACE A572 GR. 50 3.2

2 2 08-20007-203 MEMBER D SHAPED A500

GR. C 1.9

3 2 08-20007-204 PLATE, AXLE SUPPORT INTERFACE A572 GR. 50 0.3

4 2 08-20007-205 1.25-7 THREAD MATING LOCATING PIN 6061-T6 0.2

5 2 08-20007-206 ADAPTER PLATE, 2550 SINGLE ROLLER

ADAPTER, 1.00" STK A36 4.7

6 2 MODEL 2550 SINGLE ROLLER ADAPTER PLAIN

CARBON STEEL

AIR LOGISTICS

CORP

104568 /

NSN 1730-

00-986-3702 20.7

7 4 0.5625-18 X 1.000 SHCS, A574, BLACK

OXIDE GRADE 8 STEEL MCMASTER-

CARR 91251A697 0.15

8 2 08-20007-207 MEMBER A SHAPED A500

GR. C 8.0

9 2 08-20007-208 MEMBER B SHAPED A500

GR. C 17.8

10 1 08-20007-209 MEMBER C SHAPED A500

GR. C 19.2

11 4 0.5, GRADE 9, ZINC YELLOW CHROMATE

PLATED, STANDARD WASHER ALLOY STEEL MCMASTER-

CARR 90850A300 0.02

12 4 0.500-13 X 1.125 HHS, GR8, ZINC-AL

COATED GRADE 8 STEEL MCMASTER-

CARR 91286A803 0.10

13 AR LOCTITE 8150, GENERAL PURPOSE

ANTISEIZE, ALUMINUM/GRAPHITE N/A MCMASTER-

CARR 1287K51 N/A

ALL FASTENERS ARE ASSUMED TO MEET A MINIMUM

ULTIMATE TENSILE STRENGTH OF 150 KSI. A FRICTION

FACTOR OF .18 IS USED (TYPICAL FASTENERS). INTERNAL

THREADS ARE ASSUMED TO BE 6061-T6 ALUMINUM.

SIZE AND THREAD TORQUE VALUE (FT-LBS)

1/2-13 60 9/16-18 65

SHEET 1 OF 3

SEE CUTLIST

NBOC MLV

N/A

ENG.

DFT.

CHK.

DES.

CRADLE, AXLE CART, NBOC MLV

DO NOT SCALE

FROM DRAWING

THIRD ANGLE PROJECTION

125SURFACE FINISH IN

MICROINCHES RMS

(UNLESS NOTED)

TOLERANCE (INCH)

D

NEXT ASSEMBLY:

PROJECT:

1:4

SCALE:

INTERPRET PER ASME Y14.5-2009

MATERIAL:

TITLE:

DATE:

REV.08-20007-200

X.X

X.XX

X.XXX

.1

.02

.005

.25

APPROX. WEIGHT

CAGE CODE

133.9

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

18.45 CF

20.75 10.992±.063

8.

08-20007-200-XX-YY

9 2X

1 2X

2 2X

1/4

TYP 2 PLACES

TYP 2 PLACES

1.50

46.50 1.25

1.50±.01

2X 1.500

4X .609

12.992±.010

2.00

19.754±.020

2X 1-1/4-7 UNC - 2B THRU

8 2X3 2X

11.

SHEET 2 OF 3

SEE CUTLIST

NBOC MLV

N/A

ENG.

DFT.

CHK.

DES.

WELDMENT FOR CRADLE, AXLE CART,

NBOC MLV

J. BABCOCK

L. BARMOY

DO NOT SCALE

(UNLESS NOTED)

TOLERANCE (INCH)

D

SRT OPERATING UNIT

30899 PARK DRIVE

PRINCESS ANNE, MD 21853NEXT ASSEMBLY:

PROJECT:

1:4

SCALE:

INTERPRET PER ASME Y14.5-2009

MATERIAL:

TITLE:

J. BABCOCK

DATE:

REV.08-20007-200

X.X

.005

.25

APPROX. WEIGHT

CAGE CODE

SEE CUTLIST

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

Christopher Leikam Digitally signed by Christopher Leikam Date: 2024.10.08 14:44:28 -04'00'

4.00

4.00

1.60

1.60

4X R.25

1.20

1.20

PN 08-20007-202

1.0 STK

3.40 3.40

22.43

60°

2.31 9.592±.010

60°

.50 CF

PN 08-20007-209

SQ 4.00 X 4.00 X .25 WALL STK

19.00

60°

60°

PN 08-20007-208

SQ 4.00 X 4.00 X .25 WALL STK

.25

.25

1.00

2X .50

3.35

.33

9.0

60°

.25

4.00

4.00

PN 08-20007-207

SQ 4.00 X 4.00 X .25 WALL STK

2.00

2.00

.500 .250

08-20007-204

0.5 STK

1.600 1.600

.200

.200

4X R.25 5.00

PN 08-20007-203

SQ 2.00 X 2.00 X .1875 WALL STK

2.00

2.00

.188

4.00

4.00

.25 .25

4.00

4.00

.125 THRU NEARSIDE

1.500 3.250

4.00

4.53

.625

2.000

2X 1/2-13 UNC - 2B THRU ALL

2X .594 THRU ALL

1.000 .625

PN 08-20007-206

1.00" STK

.50

.571

R.050 UNDERCUT

1-1/4-7 MACHINE THREADS 2A STUD

0.05

R.571 HEMISPHERE

R.984 CF

1.25

PN 08-20007-205

SCALE 1 : 1

5.

SHEET 3 OF 3

SEE CUTLIST

NBOC MLV

N/A

ENG.

DFT.

CHK.

DES.

MACHINED DIMENSIONS FOR

CRADLE, AXLE CART, NBOC MLV

DO NOT SCALE

(UNLESS NOTED)

TOLERANCE (INCH)

D

NEXT ASSEMBLY:

PROJECT:

1:2

SCALE:

INTERPRET PER ASME Y14.5-2009

MATERIAL:

TITLE:

DATE:

REV.08-20007-200

X.X

.005

.25

APPROX. WEIGHT

CAGE CODE

SEE CUTLIST

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