NAVY MIL-R-81128-1964 ROCKET MOTORS IDENTIFICATION OF PARTS AND ASSEMBLIES REQUIREMENTS FOR《用于火箭发动机鉴定的零件和组装要求》.pdf
《NAVY MIL-R-81128-1964 ROCKET MOTORS IDENTIFICATION OF PARTS AND ASSEMBLIES REQUIREMENTS FOR《用于火箭发动机鉴定的零件和组装要求》.pdf》由会员分享,可在线阅读,更多相关《NAVY MIL-R-81128-1964 ROCKET MOTORS IDENTIFICATION OF PARTS AND ASSEMBLIES REQUIREMENTS FOR《用于火箭发动机鉴定的零件和组装要求》.pdf(6页珍藏版)》请在麦多课文档分享上搜索。
1、MIL-R-81128 (Wep)4 August 1964SupersedingOS-64279 June 1950CODE IDENT10001MILITARY SPECIFICATI ONROCKET MOTORS, IDENTIFICATION OFPARTS AND ASSEMBLIES, REQUIREMENTS FORThis specification has been approved by the Bureauof Naval Weapons, Department of the Navy1. SCOPE1.1 This specification defines gene
2、ral requirements for the markingof parts and assemblies for solid propellant rocket motors, prepackaged liquidpropellant rocket engines, and JATO units.1.2 Classification. -Marking covered by this specification shalI beof the following methods and types, as specified:MethodMethodMethodMethodMethodMe
3、thodI - Steel StampingII - Electric Etch or ScribeIll - Ink Stamp or StencilIV - DecalV - TagVI - IntegralType 1 - Component Part Marking, Non-serializedType 2- Component Part Marking, SerializedType 3- Loaded Assembly MarkingType 4- Igniter Marking2. APPLICABLE DOC UMENTS2.1 The following document
4、of the issue in effect on date of invitationfor bids form a part of this specification to the extent specified herein.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-R-81128 (WEP)SPECIFICATIONMilitary3.3.1MIL-D-8634 Decal, Elastomeric PigmentedFi
5、lm, For use on Exterior SurfacesHandbook H4-1, H4-2 Federal Supply Code for Manu-facturersREQUIREMENTSGeneral Requirements. -Marking shall comply with the followinggeneral requirements.3.1.1 Location. -The location of marking shall be as required by thedrawings. Marking by methods I and II shall not
6、 be placed nearer than 0.06inches to any corner, fillet or sharp edge.3.1.2 Sequence of Marking. -Marking shall remain visible after theapplication of final protective finish. Marking shall not mar or penetrate plating,anodizing, paint, or other protective coating. If a protective finish is broken,s
7、uitable repairs approved by the procuring activity shall be made.3.1.3 Size. -Unless otherwise specified, size of characters used formarking shall be appropriate for the part. For rocket motor assemblies, size andspacing of characters used for marking shall be as shown in Table I below:NominalUp to
8、10TABLE IMARKING SIZE FOR ROCKET MOTOR ASSEMBLIESCase Diameter Height of Lettering Spacing Between Linesinches .25 in. (.18 in. ) .25 in. .18 in. )10 inches and over .50 in. .25 in. ) .38 in. (.25 in. )NOTE: Reduced size lettering (i.e., that shown in parentheses above) may be used forsubordinate in
9、formation if necessary to conserve space. Subordinate information isdefined as that appearing below the &tted line in 3.3.3.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MlL-R-81128 (WEP)3.2.1pressed, stumped,3.2.2Method I - Steel Stamp.rolled or p
10、eened into the-Marking shall be an impression cut,part with suitable tools.Method II - Electric Etch or Scribe. -Marking shall be apermanent impression made with either an electrically operated vibratory scriber orwith an electric arc between the part and a suitable scriber.3.2.3 Method III - Ink St
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