MIL-PRF-26539 Revision G:2017
Current
The latest, up-to-date edition.
PROPELLANTS, DINITROGEN TETROXIDE
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1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
APPENDIX A - NO assay
APPENDIX B - N[2]O[4] assay
APPENDIX C - Water equivalent
APPENDIX D - Chloride
APPENDIX E - Non-volatile residue
APPENDIX F - Iron
APPENDIX G - Particulate
CONCLUIDING MATERIAL
Describes the requirements for all types and grades of dinitrogen tetroxide (N[2]O[4]) propellants.
| Committee |
FSC 9135
|
| DevelopmentNote |
Supersedes MIL P 26539 (D). (09/2004)
|
| DocumentType |
Standard
|
| Pages |
60
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
| MIL-PRF-46846 Revision D:2013 | Rubber, Synthetic, Heat - Shrinkable |
| NASA STD 6001(INT) : 2009 | FLAMMABILITY, OFFGASSING, AND COMPATIBILITY REQUIREMENTS AND TEST PROCEDURES |
| SAE AMS 2488 : 2011 | ANODIC TREATMENT - TITANIUM AND TITANIUM ALLOYS SOLUTION PH 13 OR HIGHER |
| NASA STD 6001 : 2011 | FLAMMABILITY, OFFGASSING, AND COMPATIBILITY REQUIREMENTS AND TEST PROCEDURES |
| MIL-PRF-27407 Revision D:2014 | PROPELLANT PRESSURIZING AGENT, HELIUM |
| ASTM D 1976:2013-07 | TEST METHOD FOR ELEMENTS IN WATER BY INDUCTIVELY-COUPLED ARGON PLASMA ATOMIC EMISSION SPECTROSCOPY |
| ASTM E 394 : 2015 : REDLINE | Standard Test Method for Iron in Trace Quantities Using the 1,10-Phenanthroline Method |
| MIL-PRF-25508 Revision H:2011 | PROPELLANT, OXYGEN |
| MIL-PRF-27401 Revision G:2013 | Propellant Pressurizing Agent, Nitrogen |
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