MIL-PRF-27404 Revision D:2012
Current
The latest, up-to-date edition.
Propellant, Monomethylhydrazine
English
20-04-2012
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
APPENDIX A - MONOMETHYLHYDRAZINE ASSAY
AND WATER
APPENDIX B - NON-VOLATILE RESIDUE (NVR)
Specifies the requirements for monomethylhydrazine (N[2]H[3]CH[3]) propellant.
| DevelopmentNote |
Supersedes MIL P 27404 (10/2002)
|
| DocumentType |
Standard
|
| Pages |
13
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
This specification covers the requirements for monomethylhydrazine (N2H3CH3) propellant.
| MIL-PRF-87930 Revision B:2013 | Propellant, Hydrazine - Water (70 % Hydrazine - 30 % Water) |
| MIL-PRF-26536 Revision G:2017 | Propellant, Hydrazine |
| NASA STD 6001(INT) : 2009 | FLAMMABILITY, OFFGASSING, AND COMPATIBILITY REQUIREMENTS AND TEST PROCEDURES |
| NASA MSFC STD 3535 : 2009 | STANDARD FOR PROPELLANTS AND PRESSURANTS USED FOR TEST AND TEST SUPPORT ACTIVITIES AT SSC AND MSFC |
| NASA STD 6001 : 2011 | FLAMMABILITY, OFFGASSING, AND COMPATIBILITY REQUIREMENTS AND TEST PROCEDURES |
| AIAA R 099 : 2001 | RECOMMENDED PRACTICE FOR SPACE LAUNCH INTEGRATION |
| MIL-PRF-27407 Revision D:2014 | Propellant Pressurizing Agent, Helium |
| MIL-PRF-27401 Revision G:2013 | Propellant Pressurizing Agent, Nitrogen |
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