ASTM E 595 : 2015 : REDLINE
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
Standard Test Method for Total Mass Loss and Collected Volatile Condensable Materials from Outgassing in a Vacuum Environment
10-07-2015
English
01-05-2015
CONTAINED IN VOL. 15.03, 2015 Defines a screening technique to determine volatile content of materials when exposed to a vacuum environment.
Committee |
E 21
|
DocumentType |
Redline
|
Pages |
10
|
PublisherName |
American Society for Testing and Materials
|
Status |
Superseded
|
1.1This test method covers a screening technique to determine volatile content of materials when exposed to a vacuum environment. Two parameters are measured: total mass loss (TML) and collected volatile condensable materials (CVCM). An additional parameter, the amount of water vapor regained (WVR), can also be obtained after completion of exposures and measurements required for TML and CVCM.
1.2This test method describes the test apparatus and related operating procedures for evaluating the mass loss of materials being subjected to 125°C at less than 7 × 10−3 Pa (5 × 10−5 torr) for 24 h. The overall mass loss can be classified into noncondensables and condensables. The latter are characterized herein as being capable of condensing on a collector at a temperature of 25°C.
Note 1:Unless otherwise noted, the tolerance on 25 and 125°C is ±1°C and on 23°C is ±2°C. The tolerance on relative humidity is ±5 %.
1.3Many types of organic, polymeric, and inorganic materials can be tested. These include polymer potting compounds, foams, elastomers, films, tapes, insulations, shrink tubings, adhesives, coatings, fabrics, tie cords, and lubricants. The materials may be tested in the “as-received” condition or prepared for test by various curing specifications.
1.4This test method is primarily a screening technique for materials and is not necessarily valid for computing actual contamination on a system or component because of differences in configuration, temperatures, and material processing.
1.5The criteria used for the acceptance and rejection of materials shall be determined by the user and based upon specific component and system requirements. Historically, TML of 1.00 % and CVCM of 0.10 % have been used as screening levels for rejection of spacecraft materials.
1.6The use of materials that are deemed acceptable in accordance with this test method does not ensure that the system or component will remain uncontaminated. Therefore, subsequent functional, developmental, and qualification tests should be used, as necessary, to ensure that the material's performance is satisfactory.
1.7This standard does not purport to address all of the safety concerns associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.
MIL S 24623 : B | SPLICE, FIBER OPTIC CABLE, GENERAL SPECIFICATION FOR (METRIC) |
ASTM E 1216 : 2011 : R2016 | Standard Practice for Sampling for Particulate Contamination by Tape Lift |
MIL-STD-975 Revision M:1994 | NASA STANDARD (EEE) PARTS LIST |
MIL C 31031 : 0 | CONNECTORS, ELECTRICAL, PLUGS AND RECEPTACLES, COAXIAL, RADIO FREQUENCY, HIGH RELIABILITY, FOR FLEXIBLE AND SEMIRIGID CABLES GENERAL SPECIFICATION FOR |
MIL C 24308 : C | CONNECTORS, ELECTRIC, RECTANGULAR, NON-ENVIRONMENTAL, MINIATURE, POLARIZED SHELL, RACK AND PANEL, GENERAL SPECIFICATION FOR |
MIL-STD-1246 Revision C:1994 | PRODUCT CLEANLINESS LEVELS AND CONTAMINATION CONTROL PROGRAM |
MIL-DTL-32546 Base Document:2016 | Connectors, Electrical, Circular, for High-Speed Data Bus Transmission, Copper Conductor, General Specification for |
ASTM E 2311 : 2004 : R2016 | Standard Practice for QCM Measurement of Spacecraft Molecular Contamination in Space |
ASTM D 6412/D6412M : 1999 : R2012 | Standard Specification For Epoxy (Flexible) Adhesive For Bonding Metallic And Nonmetallic Materials |
MIL-PRF-49462 Revision C:2008 | RESISTOR, FIXED, FILM, HIGH VOLTAGE, GENERAL SPECIFICATION FOR |
DOD-E-83578 Revision A:1987 | EXPLOSIVE ORDNANCE FOR SPACE VEHICLES, GENERAL SPECIFICATION FOR (METRIC) |
ASTM D 6412/D6412M:1999 | Standard Specification for Epoxy (Flexible) Adhesive for Bonding Metallic and Nonmetallic Materials |
ISO 20188:2018 | Space systems — Product assurance requirements for commercial satellites |
NASA MSFC SPEC 1238 : 2007 | THERMAL VACUUM BAKEOUT SPECIFICATION FOR CONTAMINATION SENSITIVE HARDWARE |
NASA MSFC HDBK 3575 : 2009 | OUTGASSING RATE MEASUREMENTS FOR THE SCREENING OF NONMETALLIC MATERIALS |
SAE AS12500 | Corrosion Prevention and Deterioration Control in Electronic Components and Assemblies |
ASTM E 2311 : 2004 : R2009 | Standard Practice for QCM Measurement of Spacecraft Molecular Contamination in Space |
ASTM E 1559 : 2009 | Standard Test Method for Contamination Outgassing Characteristics of Spacecraft Materials |
ASTM E 2217 : 2012 : REDLINE | Standard Practice for Design and Construction of Aerospace Cleanrooms and Contamination Controlled Areas |
EN 16603-10-04:2015 | Space engineering - Space environment |
ASTM D 6411/D6411M : 1999 : R2005 | Standard Specification for Slicone Rubber Room Temperature Vulcanizing Low Outgassing Materials |
PD IEC/TS 62861:2017 | Guidelines for principal component reliability testing for LED light sources and LED luminaires |
MIL-DTL-83513 Revision G:2008 | Connectors, Electrical, Rectangular, Microminiature, Polarized Shell, General Specification for |
IPC AJ 820 : A | ASSEMBLY AND JOINING HANDBOOK |
MIL-PRF-85045 Revision G:2014 | Cables, Fiber Optic, General Specification for |
MIL-PRF-31031 Revision C:2014 | CONNECTORS, ELECTRICAL, PLUGS AND RECEPTACLES, COAXIAL, RADIO FREQUENCY, HIGH RELIABILITY, FOR FLEXIBLE AND SEMIRIGID CABLES, GENERAL SPECIFICATION FOR |
MIL-PRF-32159 Base Document:2004 | Resistor, Chip, Fixed, Film, Zero OHM, Industrial, High Reliability, Space Level, General Specification for |
MIL-DTL-32139 Revision B:2017 | Connectors, Electrical, Rectangular, Nanominiature, Polarized Shell, General Specification for |
MIL-PRF-31032-6 Revision B:2017 | PRINTED WIRING BOARD, RIGID, SINGLE AND DOUBLE SIDED, THERMOPLASTIC RESIN BASE MATERIAL, WITH OR WITHOUT PLATED-THROUGH HOLES, FOR HIGH FREQUENCY APPLICATIONS |
IPC HDBK 850 : 0 | GUIDELINES FOR DESIGN, SELECTION AND APPLICATION OF POTTING MATERIALS AND ENCAPSULATION PROCESSES USED FOR ELECTRONICS PRINTED CIRCUIT BOARD ASSEMBLY |
IPC SM 840 : E | QUALIFICATION AND PERFORMANCE SPECIFICATION OF PERMANENT SOLDER MASK AND FLEXIBLE COVER MATERIALS |
IPC HDBK 830 : A | GUIDELINES FOR DESIGN, SELECTION AND APPLICATION OF CONFORMAL COATINGS |
MIL PRF 24308 : D | CONNECTORS, ELECTRIC, RECTANGULAR, NONENVIRONMENTAL, MINIATURE, POLARIZED SHELL, RACK AND PANEL, GENERAL SPECIFICATION FOR |
MIL-PRF-31032-5 Revision B:2017 | PRINTED WIRING BOARD, RIGID, MULTILAYERED, THERMOPLASTIC, THERMOSETTING, OR THERMOPLASTIC AND THERMOSETTING RESIN BASE MATERIAL, WITH PLATED THROUGH HOLES, FOR HIGH FREQUENCY APPLICATIONS |
MIL-PRF-55342 Revision H:2003 | RESISTOR, CHIP, FIXED, FILM, NONESTABLISHED RELIABILITY, ESTABLISHED RELIABILITY, SPACE LEVEL, GENERAL SPECIFICATION FOR |
IPC SM 840 CHINESE : E | QUALIFICATION AND PERFORMANCE SPECIFICATION OF PERMANENT SOLDER MASK AND FLEXIBLE COVER MATERIALS |
MIL-PRF-3098 Revision L:2017 | CRYSTAL UNITS, QUARTZ, GENERAL SPECIFICATION FOR |
MIL STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
MIL-DTL-3933 Revision L:2014 | Attenuators, Fixed, Space Level, Non-Space Level General Specification for |
MIL-PRF-49291 Revision D:2013 | FIBER, OPTICAL, (METRIC) GENERAL SPECIFICATION FOR |
ASTM E 2311 : 2004 | Standard Practice for QCM Measurement of Spacecraft Molecular Contamination in Space |
ASTM D 6411/D6411M:1999 | Standard Specification for Slicone Rubber Room Temperature Vulcanizing Low Outgassing Materials |
MIL-DTL-38999 Revision M:2015 | Connectors, Electrical, Circular, Miniature, High Density, Quick Disconnect (Bayonet, Threaded or Breech Coupling), Environment Resistant with Crimp Removable Contacts or Hermetically Sealed with Fixed, Solderable Contacts, General Specification for |
MIL-PRF-55182 Revision J:2017 | RESISTOR, FIXED, FILM, NONESTABLISHED RELIABILITY, ESTABLISHED RELIABILITY, AND SPACE LEVEL, GENERAL SPECIFICATION FOR |
MIL-PRF-28861 Revision E:2016 | FILTERS AND CAPACITORS, RADIO FREQUENCY/ELECTROMAGNETIC INTERFERENCE SUPPRESSION, GENERAL SPECIFICATION FOR |
SAE AMS3593B | Tubing, Plastic, Electrical Insulation Irradiated Polyvinylidene Fluoride, Semi-Rigid, Heat-Shrinkable Marker Sleeving Grade Low Outgassing |
ASTM E 1559 : 2009 : R2016 | Standard Test Method for Contamination Outgassing Characteristics of Spacecraft Materials |
I.S. EN 16603-10-04:2015 | SPACE ENGINEERING - SPACE ENVIRONMENT |
SAE AS 1701 : 2017 | LUBRICANT, SOLID FILM |
ASTM E 2352 : 2019 | Standard Practice for Aerospace Cleanrooms and Associated Controlled Environments—Cleanroom Operations |
ASTM E 1548 : 2009 : R2017 | Standard Practice for Preparation of Aerospace Contamination Control Plans |
ASTM D 4067 : 2016 : REDLINE | Standard Classification System and Basis for Specification for Reinforced and Filled Poly(Phenylene Sulfide) (PPS) Injection Molding and Extrusion Materials Using ASTM Methods |
SAE AS6021 | AS6021 Aerospace Fiber Optic Cable Assembly Drawing Specification |
ASTM E 1548 : 2009 | Standard Practice for Preparation of Aerospace Contamination Control Plans |
SAE AMS2530A | Tungsten Disulfide Coating, Thin Lubricating Film, Binder-Less Impingement Applied |
13/30295427 DC : 0 | BS IEC/PAS 61249-8-5 ED.1 - QUALIFICATION AND PERFORMANCE SPECIFICATION OF PERMANENT SOLDER MASK AND FLEXIBLE COVER MATERIALS |
BS ISO 17851:2016 | Space systems. Space environment simulation for material tests. General principles and criteria |
MIL-DTL-49292 Revision B:2006 | Cable Assemblies, Nonpressure Proof, Fiber Optic, Metric, General Specification for |
MIL-DTL-32234 Base Document:2007 | CONNECTORS, ELECTRICAL, ULTRA HIGH DENSITY, MODULAR, BLADE AND FORK, EIGHT ROW, GENERAL SPECIFICATION FOR |
SAE AMS3084C | Lubricant, Solid Film Minimal Outgassing |
BS ISO 15388:2012 | Space systems. Contamination and cleanliness control |
BS EN 16603-10-04:2015 | Space engineering. Space environment |
MIL-PRF-8805-68 Revision L:2008 | SWITCHES, SENSITIVE, SPDT, 4 AMPERES, HERMETIC SEAL |
MIL-STD-1547 Revision B:1992 | ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE VEHICLES |
PD ISO/TR 20811:2017 | Optics and photonics. Lasers and laser-related equipment. Laser-induced molecular contamination testing |
MIL C 85045 : E | CABLES, FIBER OPTICS, (METRIC), GENERAL SPECIFICATION FOR |
SAE AS39029D | Contacts, Electrical Connector, General Specification For |
ASTM D 6411/D6411M : 1999 : R2012 | Standard Specification For Silicone Rubber Room Temperature Vulcanizing Low Outgassing Materials |
ASTM D 6412/D6412M : 1999 : R2005 | Standard Specification for Epoxy (Flexible) Adhesive for Bonding Metallic and Nonmetallic Materials |
ISO 15388:2012 | Space systems — Contamination and cleanliness control |
MIL-STD-981 Revision C:2010 | DESIGN, MANUFACTURING AND QUALITY STANDARDS FOR CUSTOM ELECTROMAGNETIC DEVICES FOR SPACE APPLICATIONS |
NASA STD 6016(INT) : 2006 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
NASA STD 6016 : 2016 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
NASA STD 5017 : 2015 | DESIGN AND DEVELOPMENT REQUIREMENTS FOR MECHANISMS |
NASA HDBK 6024 : 2014 | SPACECRAFT POLYMERS ATOMIC OXYGEN DURABILITY HANDBOOK |
NASA JSC 27301 : 2009 | MATERIALS AND PROCESSES SELECTION, CONTROL, AND IMPLEMENTATION PLAN FOR JSC FLIGHT HARDWARE |
NASA PRC 5001 : 2011 | PROCESS SPECIFICATION FOR CLEANING OF HARDWARE |
IPC SM 817 : A | GENERAL REQUIREMENTS FOR DIELECTRIC SURFACE MOUNTING ADHESIVES |
SAE USCAR33 | SPECIFICATION FOR TESTING AUTOMOTIVE LED MODULES |
MIL-DTL-24308 Revision G:2009 | Connectors, Electric, Rectangular, Nonenvironmental, Miniature, Polarized Shell, Rack and Panel, General Specification for |
MIL-C-49468 Base Document:1990 | CRYSTAL UNITS, QUARTZ, PRECISION, GENERAL SPECIFICATION FOR |
MIL F 23419/11 : A | FUSES, CARTRIDGE, INSTRUMENT TYPE, STYLE FM11 (SUBMINIATURE - HIGH PERFORMANCE) |
SAE AMS3818B | Braid, Flat, Polyester, Lacing and Tying Synthetic Rubber Coated, Low Outgassing |
MIL-DTL-83733 Revision E:2006 | CONNECTORS, ELECTRICAL MINIATURE, RECTANGULAR TYPE, RACK TO PANEL, ENVIRONMENT RESISTING, 200 DEGREES C TOTAL CONTINUOUS OPERATING TEMPERATURE, GENERAL SPECIFICATION FOR |
17/30318744 DC : 0 | BS ISO 20188 - SPACE SYSTEMS - PRODUCT ASSURANCE REQUIREMENTS FOR COMMERCIAL SATELLITES |
MIL-DTL-83522 Revision E:2013 | Connectors, Fiber Optic, Single Ferrule, General Specification for |
10/30234886 DC : 0 | BS ISO 15388 - SPACE SYSTEMS - CONTAMINATION AND CLEANLINESS CONTROL |
MIL F 23419 : E | FUSE, CARTRIDGE, INSTRUMENT TYPE, GENERAL SPECIFICATION FOR |
00/705381 DC : DRAFT FEB 2000 | ISO/CD 15388 - SPACE SYSTEMS - CONTAMINATION AND CLEANLINESS CONTROL |
ASTM E 1216 : 2011 | Standard Practice for Sampling for Particulate Contamination by Tape Lift |
SAE AS85848A | Sleeving, for Identification Marking, Heat Shrinkable, General Specification for |
SAE AS85485B | Cable, Electric, Filter Line, Radio Frequency Absorptive |
ASTM E 1997 : 2015 : REDLINE | Standard Practice for the Selection of Spacecraft Materials |
IEC PAS 61249-8-5:2014 | Qualification and performance specification of permanent solder mask and flexible cover materials |
PD IEC/PAS 61249-8-5:2014 | Qualification and performance specification of permanent solder mask and flexible cover materials |
MIL-PRF-23419 Revision H:2013 | FUSE, CARTRIDGE, INSTRUMENT TYPE, GENERAL SPECIFICATION FOR |
MIL-C-29600 Base Document:1989 | CONNECTORS, ELECTRICAL, CIRCULAR, MINIATURE, COMPOSITE, HIGH DENSITY, QUICK COUPLING, ENVIRONMENT RESISTANT, REMOVABLE, CRIMP CONTACTS, ASSOCIATED HARDWARE GENERAL SPECIFICATION FOR |
NASA MSFC SPEC 1443 : 2007 | OUTGASSING TEST FOR NONMETALLIC MATERIALS ASSOCIATED WITH SENSITIVE OPTICAL SURFACES IN A SPACE ENVIRONMENT |
SAE AS6294/1 | Requirements for Plastic Encapsulated Microcircuits in Space Applications |
MIL-PRF-23419-10 Revision C:2012 | FUSES, CARTRIDGE, INSTRUMENT TYPE, STYLE FM10, (NONINDICATING) |
MIL-PRF-39007 Revision J:2005 | Resistor, Fixed, Wirewound, (Power Type) Nonestablished Reliability, Established Reliability, and Space Level General Specification for |
IPC FC 234 : A | PRESSURE SENSITIVE ADHESIVE (PSA) ASSEMBLY GUIDELINES FOR FLEXIBLE, RIGID OR RIGID-FLEX PRINTED BOARDS |
DSCC 92017 : A | GASKETS, EMI/RFI SHIELDING, EXPANDED PTFE WITH CARBON FILLER |
SAE AS5590A | Connectors, Fiber Optic, Advanced, Circular or Rectangular, Plug and Receptacle, Environment Resistant, Removable Termini/Contacts, General Specification For |
SAE AS29600B | Connectors, Electrical, Circular, Miniature, Composite, High Density, Quick Coupling, Environment Resistant, Removable Crimp Contacts Associated Hardware, General Specification For |
MIL C 83522 : D | CONNECTORS, FIBER OPTIC, SINGLE TERMINUS, GENERAL SPECIFICATION FOR |
MIL-C-83522-2 Revision G:2006 | CONNECTOR, PLUG, FIBER OPTIC, SINGLE TERMINUS, THREADED, (STRAIGHT NOSE INTERFACE), LENSLESS, EPOXY, FOR 50/125 MICROMETER, 62.5/125 MICROMETER, AND 100/140 MICROMETER |
SAE AIR 4789 : 2016 | AEROSPACE INFORMATION REPORT ON EVALUATING CORROSION TESTING OF ELECTRICAL CONNECTORS AND ACCESSORIES FOR THE PURPOSE OF QUALIFICATION |
ISO/TR 20811:2017 | Optics and photonics Lasers and laser-related equipment Laser-induced molecular contamination testing |
SAE AS85049D | Connector Accessories, Electrical General Specification For |
SAE AIR 4567 : 2014 | COMPOSITE ELECTRICAL CONNECTORS |
ASTM E 2352 : 2004 | Standard Practice for Aerospace Cleanrooms and Associated Controlled Environments-Cleanroom Operations |
ASTM E 2312 : 2011 : REDLINE | PRACTICE FOR TESTS OF CLEANROOM MATERIALS |
ASTM E 2352 : 2004 : R2010 | Standard Practice for Aerospace Cleanrooms and Associated Controlled Environments-Cleanroom Operations |
IEC TS 62861:2017 | Guidelines for principal component reliability testing for LED light sources and LED luminaires |
DSCC 03024 : C | SHIELDING BEAD, ELECTRONIC, CHIP, FERRITE, HIGH RELIABILITY |
ASTM E 177 : 2014 : REDLINE | Standard Practice for Use of the Terms Precision and Bias in ASTM Test Methods |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.