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NASA SP-R-0022

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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 ... OCR Scan
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166 pages,
19521.92 Kb

SSB-24-AA-LT J-STD-006 MIL-M-24519 NASA SP-R-0022 Omnetics Omnetics yyww PS2 series CI VERTICAL LA 7036 g vertical thru hole jack PCB Connector TEXT
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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 ... OCR Scan
datasheet

87 pages,
8461.51 Kb

SP-R-0022 J-STD-006 MIL-M-24519 nano connector NSD-44-DD-GS NSS-24-WC-18 Omnetics yyww 76357 Omnetics Connector NASA SP-R-0022 TEXT
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Abstract: ASTM-A342 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
datasheet

6 pages,
3106.13 Kb

"MIL-STD-1344" MIL-L-23649 e595 computer nasa MILDTL-83513 A342 50g a M22759 coolanol SP-R0022 Coolanol-25 MIL-STD-202 METHOD 307 M22759/11 MIL-STD-1344 method 2007 SP-R-0022 MIL-DTL-83513 MIL-STD-1344, Method 3001 MIL-STD-1344 NASA SP-R-0022 TEXT
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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
datasheet

1 pages,
52.44 Kb

TEXT
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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
datasheet

1 pages,
54.3 Kb

TEXT
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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 ... OCR Scan
datasheet

1 pages,
104.76 Kb

TEXT
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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
Original
datasheet

1 pages,
26.58 Kb

TEXT
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Abstract: MATES WITH RAYCHEM P/N 6210411 8 < TEI P/N PL3455AC PL3455AC S/P - CABLE GROUP & TEI P/N PLR3455AC 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 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
datasheet

2 pages,
60.51 Kb

QQ-S-571 305089 PL3455AC PLR3455AC SP-R-0022 TEXT
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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 ... OCR Scan
datasheet

1 pages,
51.39 Kb

2001-6005-00 NASA SP-R-0022 TEXT
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Abstract: MATERIALS MEET THE DUTGASSING REQUIREMENTS DF NASA SPECIFICATION SP-R-0022 PRE-TINNED, .0015 MAXIMUM ... OCR Scan
datasheet

1 pages,
42.93 Kb

PL345 305089 TEXT
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Archived Files

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/datasheets/files/linear/lview4/parts.edb
Linear 15/02/2000 7168.02 Kb EDB parts.edb
No abstract text available
/datasheets/files/motorola/design-n/sps/hpesd/aesop/mpc8xx/860/860um/860umsea.hqx
Motorola 12/09/1996 5721.56 Kb HQX 860umsea.hqx