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

NASA SP-R-0022

Catalog Datasheet MFG & Type PDF Document Tags
Abstract: 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 -
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g vertical thru hole jack PCB Connector CI VERTICAL LA 7036 PS2 series Omnetics yyww Omnetics MIL-M-24519 PSM-46-WD-XX PSM-33-WD-XX PSM-11-WD-18 PSM-11-WC-18
Abstract: : 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 -
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Omnetics Connector 76357 NSS-24-WC-18 NSD-44-DD-GS nano connector J-STD-006 NPD-48-WD-XX NPD-36-WD-XX NPD-48-WD-18 NPD-48-WC-18
Abstract: °C (70°F) and 50% relative humidity. Shelf Life and Storage Outgssing: (NASA SP-R-0022 or ASTM E595 3M Electronics Markets Materials
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ACF msds CONDUCTIVE INK FLEX CIRCUITS D33-30 ASTM-D3330 CONDUCTIVE INK FOR FLEX CIRCUITS dupont kapton rohs 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
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RT-555 MIL-PRF-372 SAE-AMS1424 MIL-PRF-2104 MIL-PRF-23699 MIL-PRF-46167
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
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A-A-52557 MIL-PRF-46170 MIL-PRF-5606 MIL-DTL-83133 MIL-PRF-7808
Abstract: 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
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AS22759 FED-STD-191 MIL-STD-104 wc 27500 nema wc 27500 FED-STD-228
Abstract: 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 -
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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
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
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7224 markem ZZ-R-765E/GEN
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
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Abstract: 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 -
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Markem 7224 Ink E-595
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 , 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
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Abstract: 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 -
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305089 CBBJ3459
Abstract: 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 -
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2001-6005-00 FED-STD-209
Abstract: MATERIALS MEET THE DUTGASSING REQUIREMENTS DF NASA SPECIFICATION SP-R-0022 PRE-TINNED, .0015 MAXIMUM -
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PL345 3125-32UNEF-2A DQ-S-571
Abstract: 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 -
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omni spectra sma omni spectra attenuators omni spectra sma JACK MIL-STD-202
Abstract: meet or exceed the outgassing requirements o f NASA specifications JSC SP-R-0022 for a TML of 1% max -
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MIL-D-39030 L-D-39030/3 WHL-D-39030/5 MIL-D-39030/6 L-D-39030/7 MIL-D-39030/8
Abstract: meet or exceed the outgassing requirements of NASA specifications JSC SP-R-0022 for a TML of 1% max and Midwest Microwave
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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
Abstract: the outgassing requirements of NASA specifications JSC SP-R-0022 for a TML of 1% max and a CVCM o f . -
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MIL-D-39030/3 MIL-D-39030/5 MIL-D-39030/7
Abstract: . 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
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Space Qualified Parts List
Abstract: NASA specifications JSC SP-R-0022 for a TML of 1% max and a CVCM of .1 % max. All Hi-Rel components -
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M1L-A-3933/14 MIL-A-3933/19 MIL-A-3933/18 FED-STD-201
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