NAVY MIL-B-85252-1981 BALLONET CARTRIDGE ACTIVATED (MXU-695 B)《(MXU-695 B)子弹激活气囊》.pdf
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1、MIL-B-85252(AS) T3 June 1981 MILITARY SPECIFICATION BALLONET, CARTRIDGE ACTIVATED * (MXU-695/B) This specification is approved for use by the Naval Air;Systems Command, Department of the Navy, and is available for use by all Departments and Agencies of the Department of Defense. 1. SCOPE. 1.1 Scope.
2、 This specification establishes the requirements for manu- facture and acceptance of the MXU-695/B cartridge activated ballonet, critical item, referred to herein as the ballonet. 2. APPLICABLE DOCUMENTS; 2.1 Issues of documents. The following documents of the issue in effect on date OE invitation f
3、or bids or request for proposal, form a part of this specification to the extent specified herein. SPECIFICATIONS MILITARY MIL-S-487 MIL-W-5 25 74 Sulfur, Ground (for use in Ammunition). Welding Process and Welding Procedure Requirements for Manufacture of Equipment Utilizing Steel. MIL-B-8525 1 Bom
4、b, Binary Chemical, Empty, BLU-80/B. . MIL-C-85256 Cartridge, Impulse, CCU-l3/B. Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: .Commanding Officer, Naval Air Engineering Center, Engineering Sp
5、ecifications and Standards Department (ESSD), Code 93, Lakehurst, NJ 08733, by using the self-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document, or by letter. Provided by IHSNot for ResaleNo reproduction or networking permitted without licen
6、se from IHS-,-,-STANDARDS MI LI TARY MIL-STD- 105 MIL - sm- i O 9 MIL-STD-129 MIL-STD-810 MIL-STD-45662 DRAWINGS Naval Air Systems Command (Code Ident 30003) DL X4900552 . DL X49008il SA 2875561 X49 00623 0 Sampling Procedures and Tables for Inspection by Attributes. . Quality Assurance Terms and De
7、finitions. Marking for Shipping and Storage. Environmental Test Methods. Calibration System Requirements. Ballonet, MXU-695/B. Marking, Shipping, .and Storage for MXU-695/B. Ballonet Test Fixture. Tube , Injector. (Copies of specifications, standards, drawings, and publications re- quired by contrac
8、tors in connection with specific procurement functions should be obtained from the procuring activity or as directed by the contracting officer.) 2.2 Other publications. The following documents form a part of this specification to the extent specified herein. Unless otherwise indi- cated, the issue
9、in effect on date of invitation for bids or request for proposal shall apply. DEPARTMENT OF TRANSPORTATION I. Code of Federal Regulations 49 CFR 171-178 . Transportation. (Application for copies should be addressed to the Superintendent of Documents, Government Printing Office, Washington, D.C. 2040
10、2.) 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-t b AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) ASTM-E498-73 ASTM-E499 - 7 3 STM-1778-71 Standard Methods of Testing for Leaks Using the Mass Spectrometer Leak Detector or Residual Gas Analy
11、zer in the Tracer Probe Mode. Standard Methods of Testing for Leaks Using the Mass Spectrometer Leak Detector in the Detector Probe Mode. Standard Method for Calibration of Helium Leak Detectors by use of Secondary Standards. (Applications for copies should be addressed to the American Society for T
12、esting and Materials, 1916 Race Street, Philadelphia, PA 19103.) a 3. REQUIREMENTS. 3.1 Item description. The MXU-695/B ballonet consists of a welded tube assembly and a CCU-l3/B impulse cartridge. equally spaced longitudinal depressions each approximately 50 inches long. The depressions are packed
13、with lay-flat plastic tubes filled with a mixture of sulfur and silicon dioxide. The CCU-13/B impulse . cartridge contains the propellant and ignitor for expanding the depres- sions from the tubing during operation of the weapon. The tube contains three 3.2 Characteristics. 3.2.1 Performance. 3.2.1.
14、1 Solids load. There shall be no visual evidence of white and yell.ow separation areas or lumps, and the angle of repose shall be not greater than 45 degrees (deg). 3.2.1.2 Lay-flat tubing seal. There shall be no evidence of leaks from the lay-flat tbing surface or adhesive interface (see 4.4.2). 3.
15、2.1.3 Adhesive system peel strength. The peel strength shall be not less than 75 ounces (see 4.4.3). c 3 . Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-B-S252 13 777770b 03b4075 7 4 i: . . 3.2.1.4 Tube expansion. When the CCU-l3/B impulse cart
16、ridge, in accordance with MIL-C-85256(AS), is activated, the ballonet tube shall expand to fill the inside of volume of the injector tube basket. The expansion shall cause the material contained on the ballonet to be injected through the basket due to the rupture of the scored segments of the inject
17、or tube, Drawing X4900623. The ballonet shall not exhibit leakage in excess of loe4 atmospheres cubic centimeters per second at one atmosphere differential pressure and 25 +2 degrees Celsius (OC). 3.2.2 Environmental. The ballonet performance shall not be degraded below that specified in 3.2.1, nor
18、shall there be loose or damaged parts on the ballonet, separation of the lay-flat tubing from the adhesive, separation of the adhesive from the ballonet tube, holes or cracks in the lay-flat tubing, or evidence of blend separations as shown by dis- tinct white and yellow areas, after exposure to the
19、 following environ- ments. Also, the moisture and acidity contents of the blend shall be not greater than 0.1650 and 0.0023 percent by weight, respectively. The change of angle of repose between initial and final measurements at . 50 percent relative humidity shall be no greater than 22 deg. 3.2.2.1
20、 High temperature. Exposure to a high temperature of 74OC for 48 consecutive hours (see 4.4.5). 3.2.2.2 Low temperature. Exposure to a low temperatureof -48OC for 24 consecutive hours (see 4.4.6). 3.2.2.3 Vibration: Exposure to the vibration schedule of Figure 1 in each of the three mutually perpend
21、icular axes at a temperature of -4OOC (see 4.4.7). 3.2.2.4 Shock. Exposure to half sine wave impact shocks in each of three mueualiy perpendicular.axes having a peak amplitude of 15 gravity units (8) and a total duration of 11 milliseconds (ms) (see 4.4.8). 3.2.2.5 Humidity. .Exposure to a relative
22、humidity of up to 95 percent (see 4.4.9). 3.3 Design and construction. 3 :3.1 Production drawings. The ballonet shall be fabricated and assembled in accordance with the drawings, parts list, and other docu- ments listed on DL X4900552. 3.3.2 Standards of manufacture. All materials, processes, and pa
23、rts used in the manufacture of the ballonet shall be of high quality, func- tionally suitable for the application, and shall confrm strictly to the requirements specified in applicable documents and drawings ,referenced herein. 4 Provided by IHSNot for ResaleNo reproduction or networking permitted w
24、ithout license from IHS-,-,-MIL-B-5252 13 = 3.3.2.1 Certification. When specified in the contract or purchase order, the contractor shall include written certification Co the pro- curing activity (see 6.2.2) , accompanied by ob jective quality evidence as defined in MIL-STD-109, that the materials,
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