This specification covers the requirement for nitrogen tetroxide (N2O4) solution, also known as oxidizer solution (OS) recovered from propellant systems. N2O4 solution is actually a blend of N2O4, nitric acid (HNO3), and water (H2O). This specification provides a means of categorizing recovered propellants for either reclamation for alternate reuse or for reprocessing to original manufacturing purity.
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Edition: Baseline Published: 07/10/1995 Number of Pages: 31 File Size: 1 file , 1.2 MB