AIR FORCE MIL-PRF-25604 E-1997 PROPELLANT UNS-DIMETHYLHYDRAZINE《偏二甲肼推进剂》.pdf
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1、1 H 9999906 2042437 437 MIL-PRF-25604E O1 October 97 Superseding MIL-P-25604D 23 May 1969 PERFORMANCE SPECIFICATION PROPELLANT, uns-DIMETHYLHYDRAZINE This specification is approved for use by ali Departments and Agencies of the Department of Defense 1. SCOPE 1.1 Scope. This specification covers the
2、requirements for unsymmetrical dimethylhydrazine (CH31 2NNH2 propellant (UDMH) . 2. APPLICABLE DOCUMENTS 2.1 General. The documents listed in this section are specified in sections 3 and 4 of this specification. This section does not include documents in other sections of this specification or recom
3、mended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements documents cited in sections 3 and 4 of this specification, whether or not they are listed. 2.2 Gover
4、nment documents. 2.2.1 Specifications, standards, and handbooks. The following specifications form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those listed in the issue of the Department of Defense Index of Specifications and
5、Standards (DoDISS) and supplement thereto, cited in the solicitation (see 6.2). SPECIFICATIONS FEDERAL BB-H-886 - Hydrogen BB-A-1034 - Air, Compound, for Breathing Purposes DEPARTMENT OF DEFENSE Beneficial comments (recommendations, additions, deletions) and any pertinent data.which may be of use in
6、 improving this document should be addressed to: Code (68) SA-ALC/SFSP, 1014 Billy Mitchell Blvd/STE 1, Kelly AFB TX 78241- 5603, by using the standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter. AMSC N/A FSC 9135 DISTRIBUTION STATEMENT A.
7、Approved for public release; distribution is unlimited. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-25604E MIL-PRF-27401 - Propellant Pressurizing Agent, Nitrogen MIL-PRF-27407 - Propellant Pressurizing Agent, Helium (Unless otherwise ind
8、icated, copies of the above specifications, and standards are available from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia PA 19111-5094). 2.3 Non-Government publications. The following documents form a part of this document to the extent specified herein. Un
9、less otherwise specified, the issues of the documents which are DoD adopted are those listed in the issue of the DoDISS cited in the solicitation. Unless otherwise specified, the issues of documents not listed in the DoDISS are the issues of the documents cited in the solicitation (see 6.2) . AMERIC
10、AN SOCIETY FOR .TESTING AND MATERIALS (ASTM) ASTM D 1193 - Specification for Reagent Water (DoD adopted) ASTM D 1298 - Standard Practice for Density, Relative Density (Specific Gravity), or API Gravity of Crude Petroleum and Liquid Petroleum Products by Hydrometer Method (DoD adopted) ASTM D 2276 -
11、Test Method for Particulate Contaminant in Aviation . Fuel by Line Sampling (DoD adopted) ASTM E 29 - Practice for Using Significant Digits in Test Data to Determine Conformance with Specifications (DoD adopted) (Application for copies should be addressed to the American Society for Testing and Mate
12、rials, 100 Barr Harbor Drive, West Conshohocken PA 19428-2959. 2.4 Order of preceden.ce. 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 regulat
13、ions unless a specific exemption has been obtained. 3. REQUIREMENTS 3.1 Chemical and physical properties. The chemical and physical properties of the propellant shall conform to those listed in Table I when tested in accordance.with the applicable test methods. 3.2 Limiting values. The following app
14、lies to all specified limits in this specification: For purposes of determining conformance with these requirements, an observed value or a calculated value shall be rounded off “to the nearest,unit“ in .the last right-hand digit used in expressing the specification limit according to the rounding-o
15、ff method of ASTM Practice E 29 for using Significant Digits in Test Data to Determine Conformance with Specifications. 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-II 9999906 2042439 20T MIL-PRF-25604E 3.3 Filter. A filter with a 10-micrometer
16、nominal and 40-micrometer absolute rating shall be installed between the manufacturers plant system and the container to be filled for delivery. 3.4 Qualitative. The propellant shall be colorless, homogeneous liquid when exaniined visually by transmitted light. TABLE I. Chemical and physical propert
17、ies. PROPERTIES uns-Dimethylhydrazine (Percent by weight) Water (Percent by weight) Amines (Percent by weight) N-Nitrosodimethylamine (Percent by weight) Chloride (Percent by weight) Density (g/mL) 60F Particulate (mg/L) 4. VERIFICATION LIMITS 98.0 min 0.3 max 1.5 max 0.01 max 0.003 max 0.795 to 0.7
18、97 10 max TEST PARAGRAPHS 4.3.2 4.3.2 4.3.2 4.3.6 4.3.4 4.3.5 4.3.3 4.1 Classification of inspections. The inspections shall be classified as quality conformance inspections. 4.2 Quality conformance inspection. Unless otherwise specified (6.2), each filled shipping container shall be considered a lo
19、t and shall be sampled. Each sample shall be subjected to the visual examination described in 4.3.1 for conformance to 3.4 and to the tests described in Table I for conformance to the requirements specified in Table I. 4.2.1 Sample. A sample consists of not less than 600 mL of propellant. Unless oth
20、erwise specified, quality conformance tests shall be made on the sample of propellant taken directly from the shipping container. When required, the sample shall be forwarded to a laboratory designated by the procuring activity for subjection to the quality conformance tests specified herein. The bo
21、ttle intended for sampling shall be specially cleaned and handled according to the procedure described in 4.3.3 4.2.2 Rejection. When any sample of the propellant tested in accordance with 4.3 fails to conform to the requirements specified herein, the entire lot represented by the sample shall be re
22、jected. 4.3 Test methods. 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-E 9999906 2042440 T21 m MIL-PRF-25604E 4.3.1 Examination of product. The propellant shall be visually examined while performing test specified in 4.3.3 to determine complianc
23、e with the requirement as specified herein. Examination to ensure that the material conforms to 3.4 shall be conducted after the sample has been transferred to the SOO mL calibrated cylinder. 4.3.2 Uns-Dimethylhydrazine assay, water and amines. The propellant, water, and amine content of the sample
24、shall be determined by the following method. 4.3.2.1 Gas chromatographic method. 4.3.2.1.1 Assay column preparation. Weigh 5 grams of polyethylene glycol 400 and 45 grams of 60/80 mesh Fluoropak 80 into separate beakers. Dissolve the polyethylene glycol 400 in a volume of reagent grade dichlorometha
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