AIR FORCE MIL-PRF-7254 G-1997 PROPELLANT NITRIC ACID《硝酸推进剂》.pdf
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1、MIL-PRF-7254G 15 December 1997 SUPERSEDING MIL-P-7254F 30 April 1970 PERFORMANCE SPECIFICATION PROPELLANT, NITRIC ACID This specification is approved for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specification covers the requirements for four types of
2、 nitric acid propellant. 1.2 Classification. The nitric acid will be of the following types as specified (6.2): 1.2.1 Types. The types of nitric acid are as follows: Type IIIA - Nominal 14 percent NO2 content plus corrosion inhibitor Type IIIB - Nominal 14 percent NOz content, lower solids content,
3、plus corrosion inhibitor Type IIILS - Limited storage propellant with nominal 14 percent NO2 content, lower solids content, plus corrosion inhibitor, and limited iron content Type IV - High density propellant with nominal 44 percent NO2 content, lower solids content, plus corrosion inhibitor, and li
4、mited iron content 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 recommended for additional information or as examples. While every
5、effort has been made to ensure the completeness of this list, document users are cautioned that they Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to SA- ALC/SFSP, 1014 Billy Mitchell Blvd/STE 1,
6、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. Approved for public release; distribution is unlimited. Provided by IHSNot for ResaleNo reproduction or n
7、etworking permitted without license from IHS-,-,-m 0b 2047377 927 MIL-PRF-7254G must meet all specified requirements documents cited in sections 3 and 4 of this specification, whether or not they are listed. 2.2 Government documents. 2.2.1 Specifications, standards, and handbooks. The following spec
8、ifications 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 Standards (DoDISS) and supplement thereto, cited in the solicitation (see 6.2). S P
9、ECI FICAT IONS DEPARTMENT OF DEFENSE MIL-PRF-27401 - Propellant, Pressurizing Agent, Nitrogen (Unless otherwise indicated, copies of the above specifications are available from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia.PA 19111-5094). 2.3 Non-Government p
10、ublications. The following documents form a part of this document to the extent specified herein. Unless 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 n
11、ot listed in the DoDISS are the issues of the documents cited in the solicitation (see 6.2). AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) ASTM D 1068 - Test Methods for Iron in Water (DoD adopted) ASTM E 29 - Practice for Using Significant Digits in Test Data to Determine Conformance with Speci
12、fications (DoD adopted) (Application for copies should be addressed 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 tex
13、t 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 Chemical composition and physical properties. The chemical composition and physical properties of the propellants shal
14、l conform to Table I. 3.2 Limiting values. The following applies 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 exp
15、ressing the specification limit according to the rounding-off method of ASTM Practice E 29 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. Composition “03, percent by weight NO*, percent by weight HF, percent by weight H20, percent by weight Fe20
16、3, percent by weight Solids , percent by weight, as nitrates Specific Gravity, 15.6“C/15.6“C 0 90b 2047378 863 Type IIIA Type IIIB Type IIILS Type IV Test Para 81.6 - 84.9 81.7 - 84.9 83.7 - 86.4 52.7 - 57.4 4.4.9 14 f 1 14 ? 1 14 $: 1 44 k 2 4.4.3 0.7 f 0.1 0.7 k 0.1 4.4.4 0.7 k 0.1 0.7 * 0.1 0.5 m
17、ax 4.4.8 1.5 - 2.5 1.5 - 2.5 0.5 max 4.4.7 not not 0.0015 max 0.002 max specified specified 0.10 max 0.04 max 0.04 max 0.04 max 4.4.6 4.4.5 1.564 min 1.564 min 1.572 min 1.642 min 1.575 max 1.575 max 1.582 max 1.652 max MIL-PRF-7254G for Using Significant Digits in Test Data to Determine Conformance
18、 with Specifications. 3.3 Qualitative. The propellant shall be a single phase liquid (6.4) when examined visually by transmitted light, and the IRFNA spectrum resulting from the water analysis (4.4.8 and Figure 2) shall contain the 1440 nm peak which identifies the presence of nitric acid. TABLE I.
19、Chemical composition and physical properties. 4. VERIFICATION 4.1 Classification of inspections. The inspections shall be classified as quality conformance inspections. 4.2 Quality conformance inspection. The quality conformance inspection shall consist of the following: a. Individual tests . 4.2.1
20、b. Sampling tests 4.2.2 4.2.1 Individual tests. The propellant shall be subjected to the following test as described under 4.4: Examination of product 4.4.1 4.2.2 Sampling tests. The propellant shall be selected according to 4.2.2.1 and subjected to the following tests as described under 4.3: 3 Prov
21、ided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-PRF-7254G a. Nitrogen dioxide . 4.4.3 b. Hydrogen fluoride. 4.4.4 c. Specific gravity . 4.4.5 d. Total solids . 4.4.6 e. Iron content . 4.4.7 f. Water. 4.4.8 4.2.2.1 Sampling plan. 4.2.2.1.1 s. A lot sh
22、all consist of one of the following: a. The propellant produced in not more than 24 consecutive hours from a continuous process which is used to fill shipping containers directly from the process output. A continuous process shall be the production of product by continuous input of raw materials and
23、 output of finished product by one manufacturer in one plant with no change in manufacturing conditions or materials. b. The propellant from individual runs of a batch process which is used to fill shipping containers directly from the process output. A batch process shall be the production of produ
24、ct by runs from single additions of raw materials which are reacted and purified forming the product. c. The propellant from either or both the continuous and batch processes which is held in a single storage tank and subsequently withdrawn to fill shipping containers. The product shall be homogeneo
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