MIL-DTL-19264C (OS)
DEPARTMENT OF DEFENSE STANDARDS
MIL-STD-129
Military Marking for Shipment and Storage
MIL-STD-286
Propellants, Solid; Sampling, Examination and Testing
MIL-STD-652
Propellants, Solid, For Cannons Requirements and Packing
DOD-STD-2101
Classification of Characteristics
(Copies of these documents are available online at https://assist.daps.dla.mil/quicksearch/ or from the
Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-
5094.)
2.2.2 Other Government documents, drawings, and publications. The following other Government
documents, drawings, and publications form a part of this document to the extent specified herein. Unless
otherwise specified, the issues are those cited in the solicitation or contract.
DRAWINGS
NAVAL SEA SYSTEMS COMMAND (CAGE Code 10001)
3208375
Charge, Propelling, 5-Inch, 54-Caliber, Full Mark 67 Mod 3
(Application for copies of NAVSEA drawings should be addressed to: US Navy Major Caliber
Propelling Charge AEA, Naval Surface Warfare Center Indian Head Division Picatinny Detachment,
Attn: G2, Picatinny, NJ 07806-5000.)
2.3 Non-Government publications. This section does not apply to this document.
2.4 Order of precedence. Unless otherwise noted herein or in the contract, in the event of a conflict
between the text of this document and the references cited herein the text of this document takes
precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a
specific exemption has been obtained.
3. REQUIREMENTS
First Article. When specified (see 6.2), a sample shall be subjected to first article inspection (see
3.1
6.3) in accordance with 4.4.
Composition (M101). The propellant shall meet the requirements of Table I when analyzed
3.2
(see 4.6.1).
3.3
Grain form and dimensions (M102).
3.3.1 Perforations. The grains shall be cylindrical with seven (7) evenly spaced axial perforations (see
4.6.2, 4.6.3 and 6.6).
3.3.2 Length. The length to outer diameter ratio for the grains shall be between 2.10 and 2.50 (see 4.6.2,
4.6.3 and 6.6).
Glaze. The propellant shall be glazed with graphite, MIL-G-155, Grade IV (see 4.6.3).
3.4
Integrity. The propellant grains shall be without cracks or incipient cracks between the
3.5
perforations or between the perforations and the outside edge of the grain (see 4.6.3).
2
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