MIL-DTL-82724A
specified, the issues of documents not listed in DODISS are the issues of the documents cited in the
solicitation (see 6.2).
AMERICAN SOCIETY FOR QUALITY CONTROL (ASQC)
ASQC Z1.4
Sampling Procedures and Tables for Inspection by Attributes
(Application for copies should be addressed to American Society for Quality Control, 611 East Wisconsin
Avenue, Milwaukee, WI 53202.)
AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM)
ASTM E1742
Standard Practice for Radiographic Examination (DoD Adopted)
(Application for copies of ASTMs should be sent to the American Society for Testing and Materials, 100
Barr Harbor Drive, West Conshohocken, PA 19428-2959)
2.4 Order of precedence. 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
3.1 First article. When specified (see 6.2), the contractor shall furnish sample units for first article
inspection and approval (see 4.3).
3.2 Conformance to documents. The CCU-44/B impulse cartridge shall be manufactured in accordance
with the drawings and documents listed on DL 5184850. All materials used in the manufacture of the
cartridges shall conform with the specifications referenced on the respective drawings.
3.3 Primary components. For the purpose of this specification, the header glass seal assembly (Drawing
5184834), the ignition element loaded assembly (Drawing 5184831), and the main propellant charge
(Drawing 5184839) are defined as primary components.
3.3.1 Header glass seal assembly. The header glass seal assembly shall be manufactured in accordance
with the drawings listed on DL 5184850 and undergo the tests listed in 4.6.1.
3.3.2 Ignition element. The ignition element shall be manufactured in accordance with the drawings
listed on DL 5184850 and shall meet the following requirements when tested as specified in 4.6.2.
3.3.2.1 Ignition delay time. Ignition delay time shall not exceed 10 milliseconds (see 6.3.5).
3.3.2.2 Time to maximum pressure. The time to maximum pressure shall not exceed 25 milliseconds
(see 6.3.6).
3.3.2.3 Maximum pressure. The minimum allowable value of maximum pressure shall be 2,000 psi.
3.3.3 Propellant charge.
3.3.3.1 Quantity. All propellant charges shall conform to Drawing 5184839. Charges shall be
determined by weight rather than volume measurements.
3
For Parts Inquires submit RFQ to Parts Hangar, Inc.
© Copyright 2015 Integrated Publishing, Inc.
A Service Disabled Veteran Owned Small Business