This specification covers the requirement for nitrogen tetroxide (N
2O
4) solution, also known as oxidizer solution (OS) recovered from propellant systems. N
2O
4 solution is actually a blend of N
2O
4, nitric acid (HNO
3), and water (H
2O). This specification provides a means of categorizing recovered propellants for either reclamation for alternate reuse or for reprocessing to original manufacturing purity.
| Edition : | Baseline |
| File Size : | 1
file
, 1.2 MB |
| Number of Pages : | 31 |
| Published : | 07/10/1995 |