SATPC0026847 Tab 04 SPECS.pdf
PDF 82 KB Posted
- Attached to
- Fabrication of MERCRII ECI Mechanism Components
- Solicitation number
- 80NSSC22798239Q-1
View the file
Other files
| File | Type | Posted |
|---|---|---|
| SATPC0026847 Tab 12 RFQ Open Market EXTENDED.docx | DOCX document | |
| SATPC0026847 Tab 12 RFQ Open Market Template.pdf |
On GovTribe
Work with this file
- Download the original file
- Contacts named in this file
- Similar government files
- Ask GovTribe AI about this file
Text version
4.38
OVERALL LENGTH
REF.
MARK PART WITH IDENTIFICATION NUMBER ON
(BOLD) OR ENGRAVE, PER SAE-AS478, METHOD 3B,
A A
B B
C C
D D
DO NOT SCALE DRAWING
Ball-Rod_1_1
SHEET 1 OF 1
2/2/22NJ
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:1 WEIGHT:
REVDWG. NO.
C
SIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
EXAMPLE: &DRAWING_NUMBER-001 REV &PTC_WM_REVISION
AFTER ALL MANUFACTURING PROCESSES ARE COMPLETE,
TREATMENT. THE PART IDENTIFICATION NUMBER
APPLICATION
USED ONNEXT ASSY
ALL DRAWING REQUIREMENTS, REQUIRED FOR
CONTROLLED (MACHINED) PRIOR TO ANY SURFACE
MATERIAL
SHALL BE THE DRAWING NUMBER, SERIAL NUMBER
INTERPRET GEOMETRIC
TOLERANCING PER:
ASME Y14.5M 1994PROPRIETARY AND CONFIDENTIAL
VERIFY ALL THREADED FEATURES WITH PROPER THREAD
BEGIN WITH 001.
AND THE DRAWING REVISION. SERIAL NUMBER TO
GAUGE. CHASE THREADS AS NECESSARY.
EACH INDIVIDUAL PART PRODUCED
THE INFORMATION CONTAINED IN THIS
SPECIFIED SURFACE BY LASER PER SAE-AS478-15B2
DRAWING IS THE SOLE PROPERTY OF
NASA. ANY REPRODUCTION IN PART OR
AS A WHOLE WITHOUT THE WRITTEN
PERMISSION OF NASA IS PROHIBITED.
NOTES:
MATERIAL: ALUMINUM 6061.
CERTIFICATE OF CONFORMANCE REQUIRED FOR
MATERIAL.
125 Ra ALL OVER PER ANSI/ASME B46.1 UNLESS
OTHERWISE SPECIFIED.
PART TO BE CLEAN AND FREE OF ALL DIRT,
DEBRIS, OIL, ETC.
100% INSPECTION AND DOCUMENTATION, FOR
DIMENSIONS ARE IN INCHES
TOLERANCES:
ANGULAR: 0 30'
X.X 0.03
X.XX 0.010
X.XXX 0.005
BREAK EDGES: 0.01-0.02
1.06
BOLT CIRCLE DIA
4X .20 .75
1/4-20 UNC - 2B .50
.30 X 90°, NEAR SIDE
R.06
1.750
TYP.
.03 X 45°
1.51
3.50
1.25
.010 .000
1.75
R.25
S
2.79
REF.
MARK PART WITH IDENTIFICATION NUMBER ON
(BOLD) OR ENGRAVE, PER SAE-AS478, METHOD 3B,
A A
B B
C C
D D
DO NOT SCALE DRAWING
Hinge-Pin-Snaprings_1_1
SHEET 1 OF 1
2/2/22NJ
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:1 WEIGHT:
REVDWG. NO.
C
SIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
THE INFORMATION CONTAINED IN THIS
EACH INDIVIDUAL PART PRODUCED
USED ON
AFTER ALL MANUFACTURING PROCESSES ARE COMPLETE,
EXAMPLE: &DRAWING_NUMBER-001 REV &PTC_WM_REVISION
FINISH
GAUGE. CHASE THREADS AS NECESSARY.
ALL DRAWING REQUIREMENTS, REQUIRED FOR
NEXT ASSY
AS A WHOLE WITHOUT THE WRITTEN
AND THE DRAWING REVISION. SERIAL NUMBER TO
BEGIN WITH 001.
PERMISSION OF NASA IS PROHIBITED.
VERIFY ALL THREADED FEATURES WITH PROPER THREAD
PROPRIETARY AND CONFIDENTIAL
ASME Y14.5M 1994
TOLERANCING PER:
INTERPRET GEOMETRIC
SHALL BE THE DRAWING NUMBER, SERIAL NUMBER
NOTES:
MATERIAL: ALUMINUM 6061.
CERTIFICATE OF CONFORMANCE REQUIRED FOR
MATERIAL.
125 Ra ALL OVER PER ANSI/ASME B46.1 UNLESS
OTHERWISE SPECIFIED.
PART TO BE CLEAN AND FREE OF ALL DIRT,
DEBRIS, OIL, ETC.
100% INSPECTION AND DOCUMENTATION, FOR
DIMENSIONS ARE IN INCHES
TOLERANCES:
ANGULAR: 0 30'
X.X 0.03
X.XX 0.010
X.XXX 0.005
BREAK EDGES: 0.01-0.02
A
.005
5.69
1.719+ .000
.25
5.51
DETAIL A
SCALE 4 : 1
.068+ .004 .000
TYP.
2 PLACES
1.650±.005
TYP.
2 PLACES
2.25
(BOLD) OR ENGRAVE, PER SAE-AS478, METHOD 3B,
A A
B B
C C
D D
DO NOT SCALE DRAWING
Inner-Hinge-Single_1_1
SHEET 1 OF 1
2/2/22NJ
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:1 WEIGHT:
REVDWG. NO.
C
SIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
ALL DRAWING REQUIREMENTS, REQUIRED FOR
TOLERANCING PER:
ASME Y14.5M 1994PROPRIETARY AND CONFIDENTIAL
VERIFY ALL THREADED FEATURES WITH PROPER THREAD
BEGIN WITH 001.
AND THE DRAWING REVISION. SERIAL NUMBER TO
GAUGE. CHASE THREADS AS NECESSARY.
EACH INDIVIDUAL PART PRODUCED
THE INFORMATION CONTAINED IN THIS
PERMISSION OF NASA IS PROHIBITED.
NOTES:
MATERIAL: ALUMINUM 6061.
CERTIFICATE OF CONFORMANCE REQUIRED FOR
MATERIAL.
125 Ra ALL OVER PER ANSI/ASME B46.1 UNLESS
OTHERWISE SPECIFIED.
PART TO BE CLEAN AND FREE OF ALL DIRT,
DEBRIS, OIL, ETC.
100% INSPECTION AND DOCUMENTATION, FOR
DIMENSIONS ARE IN INCHES
TOLERANCES:
ANGULAR: 0 30'
X.X 0.03
X.XX 0.010
X.XXX 0.005
BREAK EDGES: 0.01-0.02
.000
2.25
.50
1.13 1.750+ .005
R.25
3.26
4.094
.50
1.88
5.13
.50
1.13
- .015 .000
.015 + 1.031 .000-
.000
4.38
4.63
.000
2.031
.015
.015
3.31
1.81
3.094
4X .26 THRU
.31 X 90°, NEAR SIDE
.31 X 90°, FAR SIDE
2.25
(BOLD) OR ENGRAVE, PER SAE-AS478, METHOD 3B,
A A
B B
C C
D D
DO NOT SCALE DRAWING
Outer-Hinge-Single_1_1
SHEET 1 OF 1
2/2/22NJ
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:1 WEIGHT:
REVDWG. NO.
C
SIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
ALL DRAWING REQUIREMENTS, REQUIRED FOR
TOLERANCING PER:
ASME Y14.5M 1994PROPRIETARY AND CONFIDENTIAL
VERIFY ALL THREADED FEATURES WITH PROPER THREAD
BEGIN WITH 001.
AND THE DRAWING REVISION. SERIAL NUMBER TO
GAUGE. CHASE THREADS AS NECESSARY.
EACH INDIVIDUAL PART PRODUCED
THE INFORMATION CONTAINED IN THIS
PERMISSION OF NASA IS PROHIBITED.
NOTES:
MATERIAL: ALUMINUM 6061.
CERTIFICATE OF CONFORMANCE REQUIRED FOR
MATERIAL.
125 Ra ALL OVER PER ANSI/ASME B46.1 UNLESS
OTHERWISE SPECIFIED.
PART TO BE CLEAN AND FREE OF ALL DIRT,
DEBRIS, OIL, ETC.
100% INSPECTION AND DOCUMENTATION, FOR
DIMENSIONS ARE IN INCHES
TOLERANCES:
ANGULAR: 0 30'
X.X 0.03
X.XX 0.010
X.XXX 0.005
BREAK EDGES: 0.01-0.02
.000 4.125
.50
.50
1.13
1.88
4.38
3.31
.015
.000
.015 + 4.63
3.26
1.000+ .000 .015
2.063+ .015 .000
3.063+
5.13
1.81
4X .26 THRU
.005
2.25
R.25
1.750+
1.13
DO NOT SCALE DRAWING
Rod_1_1
SHEET 1 OF 1
2/2/22NJ
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:1 WEIGHT:
REVDWG. NO.
C
SIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
FINISH
ALL DRAWING REQUIREMENTS, REQUIRED FOR
CONTROLLED (MACHINED) PRIOR TO ANY SURFACE
MATERIAL
SHALL BE THE DRAWING NUMBER, SERIAL NUMBER
INTERPRET GEOMETRIC
TOLERANCING PER:
ASME Y14.5M 1994PROPRIETARY AND CONFIDENTIAL
DD
CC
BB
AA
BREAK EDGES: 0.01-0.02
(BOLD) OR ENGRAVE, PER SAE-AS478, METHOD 3B,
MARK PART WITH IDENTIFICATION NUMBER ON
BEGIN WITH 001.
AND THE DRAWING REVISION. SERIAL NUMBER TO
GAUGE. CHASE THREADS AS NECESSARY.
EACH INDIVIDUAL PART PRODUCED
THE INFORMATION CONTAINED IN THIS
PERMISSION OF NASA IS PROHIBITED.
AS A WHOLE WITHOUT THE WRITTEN
NOTES:
MATERIAL: ALUMINUM 6061.
CERTIFICATE OF CONFORMANCE REQUIRED FOR
MATERIAL.
125 Ra ALL OVER PER ANSI/ASME B46.1 UNLESS
OTHERWISE SPECIFIED.
PART TO BE CLEAN AND FREE OF ALL DIRT,
DEBRIS, OIL, ETC.
100% INSPECTION AND DOCUMENTATION, FOR
DIMENSIONS ARE IN INCHES
TOLERANCES:
ANGULAR: 0 30'
X.X 0.03
X.XX 0.010
X.XXX 0.005
1.75
2.00 R.25
TYP.
ALL EDGES
1.50
1.00
1.00
4.00
4X .26+ .01
.00 THRU
.31 X 90°, NEAR SIDE
B
4 3
ASME Y14.5M 1994
(BOLD) OR ENGRAVE, PER SAE-AS478, METHOD 3B,
C
SPECIFIED SURFACE BY LASER PER SAE-AS478-15B2
MARK PART WITH IDENTIFICATION NUMBER ON
A
C
A
AFTER ALL MANUFACTURING PROCESSES ARE COMPLETE,
DO NOT SCALE DRAWING
2/2/22
D
D
UNLESS OTHERWISE SPECIFIED:
SIZE
AS A WHOLE WITHOUT THE WRITTEN
B
NAME
SHEET 1 OF 1
DWG. NO.MATERIAL
Slot_Main_1_1INTERPRET GEOMETRIC
C
REV
TITLE:
NJ
DATE
TREATMENT. THE PART IDENTIFICATION NUMBER
NEXT ASSY
DRAWN
FINISH
WEIGHT:
ALL DRAWING REQUIREMENTS, REQUIRED FOR
SCALE: 1:1
GAUGE. CHASE THREADS AS NECESSARY.
MFG APPR.
PROPRIETARY AND CONFIDENTIAL COMMENTS:
SHALL BE THE DRAWING NUMBER, SERIAL NUMBER
ENG APPR.
AND THE DRAWING REVISION. SERIAL NUMBER TO
BEGIN WITH 001.
CHECKED
TOLERANCING PER:
THE INFORMATION CONTAINED IN THIS
CONTROLLED (MACHINED) PRIOR TO ANY SURFACE
APPLICATION
Q.A.
PERMISSION OF NASA IS PROHIBITED.
NOTES:
MATERIAL: ALUMINUM 6061.
CERTIFICATE OF CONFORMANCE REQUIRED FOR
MATERIAL.
125 Ra ALL OVER PER ANSI/ASME B46.1 UNLESS
OTHERWISE SPECIFIED.
PART TO BE CLEAN AND FREE OF ALL DIRT,
DEBRIS, OIL, ETC.
100% INSPECTION AND DOCUMENTATION, FOR
DIMENSIONS ARE IN INCHES
TOLERANCES:
ANGULAR: 0 30'
X.X 0.03
X.XX 0.010
X.XXX 0.005
BREAK EDGES: 0.01-0.02
3.00
2.00
5.00
2.75
.88
7.50
.30 X 90°, NEAR SIDE
2.25
1.75
2X .20 .65
1/4-20 UNC - 2B .50
.50
2.64
3.50
.86
R.25
.50
7.50
8.00
4X .26 THRU
(BOLD) OR ENGRAVE, PER SAE-AS478, METHOD 3B,
A A
B B
C C
D D
DO NOT SCALE DRAWING
Slot_Plate_1_1
SHEET 1 OF 1
2/2/22NJ
UNLESS OTHERWISE SPECIFIED:
SCALE: 1:1 WEIGHT:
REVDWG. NO.
C
SIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
PROPRIETARY AND CONFIDENTIAL TOLERANCING PER:
THE INFORMATION CONTAINED IN THIS
DRAWN
PERMISSION OF NASA IS PROHIBITED.
GAUGE. CHASE THREADS AS NECESSARY.
FINISH
EXAMPLE: &DRAWING_NUMBER-001 REV &PTC_WM_REVISION
AFTER ALL MANUFACTURING PROCESSES ARE COMPLETE,
USED ON
INTERPRET GEOMETRIC
BEGIN WITH 001.
AND THE DRAWING REVISION. SERIAL NUMBER TO
SHALL BE THE DRAWING NUMBER, SERIAL NUMBER
AS A WHOLE WITHOUT THE WRITTEN
NEXT ASSY
DRAWING IS THE SOLE PROPERTY OF
ALL DRAWING REQUIREMENTS, REQUIRED FOR
ASME Y14.5M 1994
NOTES:
MATERIAL: ALUMINUM 6061.
CERTIFICATE OF CONFORMANCE REQUIRED FOR
MATERIAL.
125 Ra ALL OVER PER ANSI/ASME B46.1 UNLESS
OTHERWISE SPECIFIED.
PART TO BE CLEAN AND FREE OF ALL DIRT,
DEBRIS, OIL, ETC.
100% INSPECTION AND DOCUMENTATION, FOR
DIMENSIONS ARE IN INCHES
TOLERANCES:
ANGULAR: 0 30'
X.X 0.03
X.XX 0.010
X.XXX 0.005
BREAK EDGES: 0.01-0.02
.50
2.25
1.38 .25
8.00
7.50
5.00
3.00
4X .26 THRU
.31 X 90°, NEAR SIDE
.86
.88
DEPTH
SPECIFIED SURFACE BY LASER PER SAE-AS478-15B2
UNLESS OTHERWISE SPECIFIED:
(BOLD) OR ENGRAVE, PER SAE-AS478, METHOD 3B,
A A
B B
C C
D D
MARK PART WITH IDENTIFICATION NUMBER ON
Socket_1_1
SHEET 1 OF 1
2/2/22
DO NOT SCALE DRAWING
REV
SCALE: 1:1 WEIGHT:
NJ
DWG. NO.
C
SIZE
TITLE:
NAME DATE
COMMENTS:
Q.A.
MFG APPR.
ENG APPR.
CHECKED
DRAWN
THE INFORMATION CONTAINED IN THIS
AFTER ALL MANUFACTURING PROCESSES ARE COMPLETE,
EXAMPLE: &DRAWING_NUMBER-001 REV &PTC_WM_REVISION
FINISH
GAUGE. CHASE THREADS AS NECESSARY.
ALL DRAWING REQUIREMENTS, REQUIRED FOR
NEXT ASSY
AS A WHOLE WITHOUT THE WRITTEN
AND THE DRAWING REVISION. SERIAL NUMBER TO
BEGIN WITH 001.
PERMISSION OF NASA IS PROHIBITED.
PROPRIETARY AND CONFIDENTIAL
ASME Y14.5M 1994
TOLERANCING PER:
INTERPRET GEOMETRIC
SHALL BE THE DRAWING NUMBER, SERIAL NUMBER
NOTES:
MATERIAL: ALUMINUM 6061.
CERTIFICATE OF CONFORMANCE REQUIRED FOR
MATERIAL.
125 Ra ALL OVER PER ANSI/ASME B46.1 UNLESS
OTHERWISE SPECIFIED.
PART TO BE CLEAN AND FREE OF ALL DIRT,
DEBRIS, OIL, ETC.
100% INSPECTION AND DOCUMENTATION, FOR
DIMENSIONS ARE IN INCHES
TOLERANCES:
ANGULAR: 0 30'
X.X 0.03
X.XX 0.010
X.XXX 0.005
BREAK EDGES: 0.01-0.02
SECTION C-C
3.75
TYP.
1.25
2.50
.25
S 1.750+ .010
.03 X 45° R.03
.31 X 90°, FAR SIDE
4X .26 THRU
.31 X 90°, NEAR SIDE
3.13
BOLT HOLE CIRCLE DIA
CC
| Ball-Rod_1_1 - Sheet1 |
| Hinge-Pin-Snaprings_1_1 - Sheet |
| Inner-Hinge-Single_1_1 - Sheet1 |
| Outer-Hinge-Single_1_1 - Sheet1 |
| Rod_1_1 - Sheet1 |
| Slot_Main_1_1 - Sheet1 |
| Slot_Plate_1_1 - Sheet1 |
| Socket_1_1 - Sheet1 |
File details come from the government source that posted it. Updated .