NAVY MIL-T-7743 F-1993 TESTING STORE SUSPENSION AND RELEASE EQUIPMENT GENERAL SPECIFICATION FOR《存储悬架和释放设备测试的一般规格》.pdf
《NAVY MIL-T-7743 F-1993 TESTING STORE SUSPENSION AND RELEASE EQUIPMENT GENERAL SPECIFICATION FOR《存储悬架和释放设备测试的一般规格》.pdf》由会员分享,可在线阅读,更多相关《NAVY MIL-T-7743 F-1993 TESTING STORE SUSPENSION AND RELEASE EQUIPMENT GENERAL SPECIFICATION FOR《存储悬架和释放设备测试的一般规格》.pdf(53页珍藏版)》请在麦多课文档分享上搜索。
1、3 INCH-POUND 30 April 1993 SUPERSEDING MIL-T-7743F MIL-T-7743E 8 October 1976 MILITARY SPECIFICATION TESTING, STORE SUSPENSION AND RELEASE EQUIPMENT, GENERAL SPECIFICATION FOR This specification is approved for use by all Departments and Agencies of the Department of Defense. l. SCOPE , 1.1 Scope. T
2、his specification covers laboratory tests to be used in W determining the suitability of all types of store suspension equipment intended for military aircraft use. 2. APPLICABLE DOCUMENTS 2.1 Government documents. 2.1.1 Specifications, standards and handbooks. The following specifica- a tions, stan
3、dards and handbooks 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 Standard (DODISS) and supplement thereto, cited in the solicitation (see 6
4、.2). SPECIFICATIONS MILITARY MIL-E-6051 MILITARY MI L-STD-461 Electromagnet Standards Electromagnet Requirements Interference ic Compatibility Requirements, System IC Emissions and Suscepti bi 1 i ty for the Control of Electromagnetic MI L-STD-704 Aircraft Electric Power Characteristics Beneficial c
5、omments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: Commanding Officer, Naval Air Warfare Center Aircraft Division Lakehurst, Systems Requirements Department, Code SR3, Lakehurst, NJ 08733-5100, by using the se
6、lf-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter. AMSC NIA FSC 6635 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Provided by IHSNot for ResaleNo reproduction or networking permitted witho
7、ut license from IHS-,-,-flIL-T-77Y3F m 93399Ob L85139b YbT m MIL-T-7743F MI L-STD- 1 385 Preclusion of Ordnance Hazards in Electro- magnetic Fields; General Requirements for HANDBOOKS MI LI TARY MIL-HDBK-235-1, -2, -3 Electromagnetic (Radiated) Environment Con- siderations for Design and Procurement
8、 of Electrical and Electronic Equipment, Subsystems and Sys tems (Unless otherwise indicated, copies of federal and military specifications, standards and handbooks are available from DODSSP - Customer Service, Standardization Documents Order Desk, 700 Robbins Avenue, Bldg. 4D, Philadelphia, PA 1911
9、1-5094.) 2.2 Non-Government publications. The fol lowing document(s1 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 spec
10、ified, the issues of documents not listed in the OODISS are the issues of the documents cited in the solicitation (see 6.2). AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) ASTM B 117 Standard Test Method of Salt Spray (Fog) Testing (Application for copies should be addressed to the American Socie
11、ty for Testing and Materials, 1916 Race Street, Philadelphia, PA 19103-1137.) (Non-Government standards and other publications are normally available from the organizations that prepare or distribute the documents. These documents also may be available in or through libraries or other informational
12、servi ces. 1 2.3 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.
13、 3. REQUIREMENTS 3.1 Test condition tolerance. Tolerance is defined as the range of indicated values taken from test instruments having errors as specified in 3.2. Unless otherwise specified, test condition tolerances shall be as follows, exclusive of thermocouple accuracy: a. Tolerances for use wit
14、h test chambers: l. Air temperature at the control sensor: +2.8“C (25F) in the range of -73.3“ to 93.3“C (-100“ to ZOOOF). For other temperatures, the tolerance shall be 23 percent of the indicated value of temperature in “C. 2 Provided by IHSNot for ResaleNo reproduction or networking permitted wit
15、hout license from IHS-,-,-flIL-T-7743F m 999990b 1851397 3Tb m MI L-T-7743F 2. Pressure: When measured by devices such as manometers, +S percent or +1.5 mm (0.059 inches) of mercury, whichever provides th greater accuracy. When measured by devices such as ion gages, 210 percent to Torr. 3. Relative
16、humidity at the control sensor: 25 percent. b. Other tolerances: l. Vi bration amp1 i tude: Sinusoidal, 210 percent. 2. Vibration frequency: - +2 percent, or 21 12 Hz below 20 Hz. 3. Acceleration or shock: 210 percent. 4. Dive or climb attitude: 53 degrees. 5. Torque: - +5 percent. 6. Di stance: - +
17、1/32 inch. 3.2 Error of test instruments. The error (inaccuracy) ments shall be equal to or better than the tolerances specif of test instru- ied in 3.1. 3.3 Inspection conditions. Unless otherwise specified, all inspections shall be performed under the fol lowing conditions : a. Test temperature. U
18、nless otherwise specified, the test temperature, hereafter designated room temperature, shall be 25“ 2 10C (77“ 2 18F). At other temperatures specified, the tolerance shall be 22.8“C (25F). All parts of the item shall be stabi lized at the specified temperature prior to conducting any tests. Unless
19、otherwise specified, temperature stabil iza- tion wi 11 have been attained when the temperature of the surface of the largest mass of the item does not change more than 22.8“C (25F) per hour. b. Test voltage. Unless otherwise specified, the nominal test voltages, at the item terminals or connectors,
20、 shall be 115 2 10 volts root mean square (rms) line-to-neutral for the 115/200 volt alternating current (Vac) system and 28 2 2 volts line-to-ground for the 28 volt direct current (Vdc) system. However, the item shall operate satisfactorily between the voltage limits as specified in MIL-STD-704. Wh
21、ere an electrical pulse is specified herein, the tolerance of the duration of the pul se shall be 210 percent or 0.002 second, whichever is greater. c. Test attitude. Unless otherwise specified, the test shall be conducted in an attitude simulating horizontal level flight, with the item mounted in a
22、 manner simi lar to that used in mounting the i tem in the aircraft. d. Sway braces. Unless otherwise specified by the acquiring activity, release tests on the item shall be conducted with the sway braces adjusted to preload values specified in the items 3 Provided by IHSNot for ResaleNo reproductio
23、n or networking permitted without license from IHS-,-,-MIL-T-7793F 9 9999906 L85L398 232 9 MI L-T-7743F service manual, or item detailed specification, or as directed by the acquiring activity. 3.4 Auxiliary equipment. When the item is operated in conjunction with separate, stand-alone mechanisms su
24、ch as inflight locks, electric fuzes, arming units, or solenoid releases, tests shall be conducted with prequalified mechanisms only. The acquiring activity, however, reserves the right to permit the use of unqualified mechanisms. All tests of section 4 pertaining to detent stylelspring loaded ball
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