500 MILLION PARTS FROM 12000 MANUFACTURERS

DATASHEET SEARCH ENGINE

Top Results

Part Manufacturer Description Datasheet BUY
2-1520230-3 TE Connectivity / Alcoswitch 8909K27=20A TOG NASA visit Digikey Buy
MAX9919NASA+T Maxim Integrated Products Operational Amplifier, 1 Func, 1300uV Offset-Max, BICMOS, PDSO8, ROHS COMPLIANT, MS-012, SOIC-8 visit Digikey Buy
MAX31855NASA+ Maxim Integrated Products Analog Circuit, 1 Func, PDSO8, ROHS COMPLIANT, SOP-8 visit Digikey Buy
MAX9919NASA+ Maxim Integrated Products Operational Amplifier, 1 Func, 1000uV Offset-Max, BICMOS, PDSO8, 0.150 INCH, ROHS COMPLIANT, MS-012A1, SOIC-8 visit Digikey Buy
MAX31855NASA+T Maxim Integrated Products Analog Circuit, 1 Func, PDSO8, ROHS COMPLIANT, SOP-8 visit Digikey Buy
208262-3 TE Connectivity Ltd 5009-328-0022 visit Digikey Buy

NASA SP-R-0022

Catalog Datasheet MFG & Type PDF Document Tags

g vertical thru hole jack PCB Connector

Abstract: PS2 series microsecond Thermal Vacuum Outgassing: NASA SP-R-0022 Contact Resistance: 26 milliohms (65 mv) max @ 2.5 , g's discontinuity , microsecond Vibration: 20 g's discontinuity , , microsecond Thermal Vacuum Outgassing: NASA SP-R-0022 Contact Resistance: 26 milliohms (65 mv) max @ 2.5
-
OCR Scan
g vertical thru hole jack PCB Connector PS2 series Omnetics yyww J-STD-006 MIL-M-24519 MB48 PSM-46-WD-XX PSM-33-WD-XX PSM-11-WD-18 PSM-11-WC-18

NASA SP-R-0022

Abstract: Omnetics Connector : 20 g's discontinuity , nanoseconds Thermal Vacuum Outgassing: NASA SP-R-0022 Contact Resistance: 71 milliohms (71 mv) max @ 1 amp , nanoseconds Thermal Vacuum Outgassing: NASA SP-R-0022 Contact Resistance: 71 milliohms (71 mv) max @ 1 amp , -24519 Socket: Gold Plated Copper Alloy Encapsulant: Epoxy Thermal Vacuum Outgassing: NASA SP-R-0022 , : 20 g's discontinuity
-
OCR Scan
NASA SP-R-0022 Omnetics Connector 76357 nano connector NSD-44-DD-GS NSS-24-WC-18 NPD-48-WD-XX NPD-36-WD-XX NPD-48-WD-18 NPD-48-WC-18

ACF msds

Abstract: NASA SP-R-0022 °C (70°F) and 50% relative humidity. Shelf Life and Storage Outgssing: (NASA SP-R-0022 or ASTM E595
3M Electronics Markets Materials
Original
ACF msds D33-30 CONDUCTIVE INK FLEX CIRCUITS ASTM-D3330 dupont kapton rohs ideas 225-3S-06
Abstract: 6 NASA SP-R-0022 General Specification, Vacuum Stability Requirements of Polymeric Material , ASTM D 2671 ASTM D 792 Section 4.3.3 Section 4.3.4 Section 4.3.5 Section 4.3.2 ASTM D 2671 NASA Raychem
Original
RT-555 MIL-PRF-372 SAE-AMS1424 MIL-PRF-2104 MIL-PRF-23699 MIL-PRF-46167

A-A-52557

Abstract: http://www.iso.ch/iso/en/ISOOnline.frontpage NASA SP-R-0022 General Specification, Vacuum , Section 4.3.2 ASTM D 2671 NASA Specification SP-R-0022A Section 4.3.6 Section 4.3.2 ASTM D 2671
Tyco Electronics
Original
A-A-52557 MIL-PRF-46170 MIL-PRF-5606 MIL-DTL-83133 MIL-PRF-7808

FED-STD-191

Abstract: AS22759 of 20 National Aeronautics and Space Administration (NASA) SP-R-0022 General Specification for Vacuum Stability Requirements of Polymeric Material for Spacecraft Application (Copies of NASA , (CVCM) shall not exceed 0.10 percent. These requirements comply with NASA Specification SP-R-0022. 4
Tyco Electronics
Original
AS22759 FED-STD-191 MIL-STD-104 nema wc 27500 wc 27500 Sample form for INCOMING Inspection of RAW MATERIAL

NASA SP-R-0022

Abstract: MIL-STD-1344 E Outgassing 1.0% Total Mass Loss (TML) SP-R-0022 (NASA) or ASTM E595 0.1% total , n Applications Outgassing 1.0% Total Mass Loss (TML) SP-R-0022 (NASA) or ASTM E595
-
Original
MIL-STD-1344 MIL-DTL-83513 M22759/11 MIL-L-23649 MIL-STD-1344, Method 3001 MIL-STD-1344 method 2007 MIL-STD-202 METHOD 307 MIL-STD--202 M22759/33

7224 markem

Abstract: 4 Space qualified connectors Outgassing Requirements for Space Rated Connectors. Trompeter has a long and proud history of servicing space applications. NASA uses the specification (SP-R-0022), Vacuum Stability Requirements of Polymeric Material for Space Application, to qualify materials for use , to as Total Mass Loss, or TML. Under the NASA specification, the material's TML should not exceed , matter that condenses and collects on a surface. Under the NASA specification, the maximum condensable
Trompeter Electronics
Original
7224 markem ZZ-R-765E/GEN

7224 markem

Abstract: 4 Space qualified connectors Outgassing Requirements for Space Rated Connectors. Trompeter has a long and proud history of servicing space applications. NASA uses the specification (SP-R-0022), Vacuum Stability Requirements of Polymeric Material for Space Application, to qualify materials for use , to as Total Mass Loss, or TML. Under the NASA specification, the material's TML should not exceed , matter that condenses and collects on a surface. Under the NASA specification, the maximum condensable
Trompeter Electronics
Original

7224 markem

Abstract: Markem 7224 Ink S pace qualified connectors Outgassing Requirements for Space Rated Connectors. Trompeter has a long and proud history of servicing space applications. NASA uses the specification (SP-R-0022), Vacuum Stability Requirements of Polymeric Material for Space Application, to qualify materials for use , to as Total Mass Loss, or TML. Under the NASA specification, the material's TML should not exceed , matter that condenses and collects on a surface. Under the NASA specification, the maximum condensable
-
OCR Scan
Markem 7224 Ink E-595

1/Markem 7224 Ink

Abstract: 7224 markem 4 Space-qualified connectors Outgassing Requirements for Space Rated Connectors Trompeter has a long and proud history of servicing space applications. NASA uses the specification (SP-R-0022), Vacuum Stability Requirements of Polymeric Material for Space Application, to qualify materials for use , Total Mass Loss, or TML. Under the NASA specification, the material's TML should not exceed 1.0% of the , condenses and collects on a surface. Under the NASA specification, the maximum condensable material allowed
Trompeter Electronics
Original
1/Markem 7224 Ink Markem+7224+Ink

QQ-S-571

Abstract: 305089 MATES WITH RAYCHEM P/N 6210411 8 < TEI P/N PL3455AC S/P - CABLE GROUP & TEI P/N PLR3455AC S/P - CABLE GROUP ALL MATERIALS MEET THE OUTGASSING REQUIREMENTS F NASA SPECIFICATION SP-R-0022 PRE-TINNED, .0015 MAXIMUM THICKNESS WITH SN53 DR EQUIV SOLDER, PER QQ-S-571, TO WITHIN ,060 MAXIMUM UF SHOULDER, AFTER PLATING 3. 2. MAX PANEL THK .125 CONCENTRIC TWINAX NONINSULATED CIRCUIT BOARD BULKHEAD MOUNT RECEPTACLE, WITH PIN DR SOCKET INTERMEDIATE CDNTACT AND SDCKET OR PIN CENTER CONTACT, DUTGASSED FDR SPACE
-
OCR Scan
305089 CBBJ3459

NASA SP-R-0022

Abstract: 2001-6005-00 non-metal materials utilized in Hi-Rel terminations meet the outgassing requirements of NASA specification JSC SP-R-0022 for a TML of 1% max. and a CVCM of .1% max. In-Process Inspections Contact Engaging
-
OCR Scan
2001-6005-00 FED-STD-209

305089

Abstract: NASA SP-R-0022 MATERIALS MEET THE DUTGASSING REQUIREMENTS DF NASA SPECIFICATION SP-R-0022 PRE-TINNED, .0015 MAXIMUM
-
OCR Scan
PL345 3125-32UNEF-2A DQ-S-571

omni spectra sma

Abstract: omni spectra attenuators Space Qualified Mj !MX>M Omni Spectra manufactures High Reliability (Hi-Rel) attenuators suitable for space flight. These attenuators incorporate EMI tight captivation techniques for the connectors, and complete traceability for all piece parts utilized in their construction. All non-metal materials utilized in the construction of Hi-Rel products meet or exceed the outaeffising requirements of NASA specifications JSC SP-R-0022 for a TML of 1% max. and a CVCM of .1% max. In-Process Inspections Sample Size
-
OCR Scan
omni spectra sma omni spectra attenuators omni spectra sma JACK MIL-STD-202

MIL-D-39030

Abstract: meet or exceed the outgassing requirements o f NASA specifications JSC SP-R-0022 for a TML of 1% max
-
OCR Scan
MIL-D-39030 L-D-39030/3 WHL-D-39030/5 MIL-D-39030/6 L-D-39030/7 MIL-D-39030/8
Abstract: the outgassing requirements of NASA specifications JSC SP-R-0022 for a TML of 1% max and a CVCM o f . -
OCR Scan
MIL-D-39030/3 MIL-D-39030/5 MIL-D-39030/7

MIL-A-3933

Abstract: MILA-3933 meet or exceed the outgassing requirements of NASA specifications JSC SP-R-0022 for a TML of 1% max and
Midwest Microwave
Original
MIL-A-3933 MILA-3933 16SMA JSC SP-R-0022 MIL-A-3933/25 MIL-A-3933/14 MIL-A-3933/16 MIL-A-3933/24 MIL-A-3933/17

MIL-D-39030

Abstract: Space Qualified Parts List . All non-metal materials used meet or exceed the outgassing requirements of NASA specifications JSC SP-R-0022 for a TML of 1% max and a CVCM of .1% max. All Hi-Rel components are manufactured in a clean
Midwest Microwave
Original
Space Qualified Parts List

MIL-A-3933

Abstract: NASA specifications JSC SP-R-0022 for a TML of 1% max and a CVCM of .1 % max. All Hi-Rel components
-
OCR Scan
M1L-A-3933/14 MIL-A-3933/19 MIL-A-3933/18 FED-STD-201
Showing first 20 results.