MIL-PRF-26536F
4.3.5 Iron. The iron content of the propellant shall be determined by one of the methods
described in Appendix C. In case of a dispute, the atomic absorption method (C.2.1) shall be the referee.
4.3.6 Non Volatile Residue (NVR). The nonvolatile residue of the propellant shall be determined
in duplicate by either of the methods in Appendix D. In case of a dispute, the dropwise method
(D.2.1) shall be the referee.
4.3.7 Aniline. The aniline content of the propellant shall be determined by one of the methods
found in Appendix E. In case of a dispute the spectrophotometric method (E.2.1) and the wide bore
capillary method (E.2.3) shall be the referee methods for monopropellant and high purity grades
respectively
4.3.8 Carbon dioxide. The carbon dioxide content of hydrazine shall be determined by one of
the methods described in Appendix F. In case of a dispute, the gas chromatographic method (F.2.1) shall
be the referee.
4.3.9 Other volatile carbonaceous material (OVCM). Other volatile carbonaceous material shall
be determined by the gas chromatographic method found in Appendix G.
5. PACKAGING
5.1 Packaging. For acquisition purposes, the packaging requirements shall be as specified in
the contract or order (see 6.2). When actual packaging of materiel is to be performed by DoD or in-house
contractor personnel, these personnel need to contact the responsible packaging activity to ascertain
packaging requirements. Packaging requirements are maintained by the Inventory Control Point's
packaging activities within the Military Service or Defense Agency, or within the Military Service's System
Commands. Packaging data retrieval is available from the managing Military Department's or Defense
Agency's automated packaging files, CD-ROM products, or by contacting the responsible packaging
activity.
6. NOTES
(This section contains information of a general or explanatory nature that may be helpful, but is not
mandatory.)
6.1 Intended Use. The propellant described by this specification is intended for use as a fuel in
rocket engines.
6.2 Acquisition requirements. Acquisition documents must specify the following:
a. Title, number, and date of this specification.
b. Grade of the propellant required (see 1.2).
c. Method of shipment, type and capacity of containers.
d. Quantity by weight.
e. When a different sampling plan is required (see 4.2.2.1).
f. Packaging requirements (see 5. 1).
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