AIR FORCE MIL-C-27410-1966 COMPONENTS ROCKET PROPULSION FLUID SYSTEM GENERAL SPECIFICATION FOR《火箭推进流体系统部件的一般规定》.pdf
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1、MIL-C-27410 = 9999906 1741302 55 W MIL-C-27410(USAF) 15 November 1966 MILITARY SPECIFICATION COMPONENTS, ROCKET PROPULSION FLUID SYSTEM, GENERAL SPECIFICATION FOR 1. SCOPE 1.1 Scope. This specification covers the requirements and instruc- tions for preparation of the manufacturers mode specification
2、 for all components of a rocket propulsion system which control the pressure or flow of ullage, gas, pressurizing gas, propellants, combustion products, or hydraulic f hid. Specifically excluded from this specification are tankage, turbo machinery, injectors, thrust chambers, nozzles, and gas genera
3、tors. 2. APPLICABLE DOCUMENTS. 2.1 The following documents of the issue in effect on date of invitation for bids or request for proposal, form a part of this cpeci- fication to the extent specified herein. SPECIFICATIONS Military MIL-P-116 Preservation, Methods of MIL-D-1000 Drawings, Engineering an
4、d Associated Lists MIL-S-4040 Solenoid, Electrical, General Specifi- cation For MIL-E-5272 MIL-C-6021 MIL-1-6181 Environmental Testing, Aeronautical and Associated Equipment, General Specification For Castings, Classification and Inspection of Interference Control Requirements, Aircraft Equipment MI
5、L-P-6906 Plates, Identification MIL-S-7 742 Screw Threads, Standard, Optimum Selected Series; General Specifi- cation For - - Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-27430 M 9999906 3743303 791 MIL-C-27410 (USAF) 1 NIL-W-8160 mL-E-8189
6、MIL-S-8879 MIL-M- 9 95 O MIL-N-25027 %IL-E-25366 MIL-H-25475 MIL-P-2 7 4 07 MIL-P-27409 STANDARDS Military ?lIL-STD-129 MIL-STD-130 MIL-STD-143 MIL-STD-446 MIL-STD-454 MIL-STD-785 Wirina, Guided Yissile, Installation of, General Specification For Electronic Equipment, Guided Missiles, General Specif
7、ication For Screw Threads, Controlled Radius Root with Increased Minor Diameter: General Specification For Missile Component, Liquid Oxygen Nitrogen Gaseous Oxygen, Instrument Air, Helium and Fuel Handling Systems, Cleaning and Packaging for Delivery Nut, Self-Locking, 250 Deg. F, 450 Deg. F, and 80
8、0 Deg. F, 125 KCI FTU, 60 KSI FTU, and 30 KSI PTU Electric and Electronic Equipment and Systems, Guided Xissiles, Installation of, General Specification For Hydraulic Systems, Xissile. Design, Installation Tests, and Data Require- ments, General Requirements For Propellant, Pressurizing Agent, Heliu
9、m Propellant Feed System, Rocket Propulsion, General Specification For Marking for Shipment and Storage Identification Harking of U. S. Military Property Specifications and Standards Order of Precedence for the Selection of Environment or Electronic Parts, Tubes and Solid State Devices Standard Gene
10、ral Requirements for Electronic Equipment Reliability ProKram for Systems, Subsystems, and Equipment 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-_ - MIL-C-27410 9 9999906 1741304 628 MIL-STD-810 Environmental Test Fkthods for Aerospace and Grou
11、nd Equipment MS 33540 Safety Wiring, General Practices For MS 33588 Nuts and Plate Nuts, Self-Locking, Air- craft Design and Usage Limitations of PUBLICATIONS Air Force - Navy Aeronautical Bulletins No. 343 No. 438 No. 445 Specifications and Standards Applicable to Aircraft Engines and Propellers, U
12、se of Age Controls of Age-Sensitive Elastomeric Items Engineering Changes to Weapons, Systems, Equipment , and Facilities 3, REQUIREI.IENTS 3.1 General. 3.1.1 Model specifications. A model specification conforming to the Appendix specified herein shall be prepared by the contractor or nianufac- ture
13、r for approval by the procuring activity (6.3.8). 3.1.2 Pre-production. Prior to initiating production of components for use in f lght systems components shall have suecescfully completed the Qualification tests (4.2.2). 3.1.3 Changes. The contractor shall notify the procuring acclvi.ty of any propo
14、sed design changes to the component as defined in the model speci- fication. Following successful completion of the Qualification tests, no change shall be made except when such changes are made in accordance with ANA Bulletin No. .445 or procurement activity requirements as applicable. Approval of
15、changes does not relieve the contractor from full responsibility for the effects of the changes on the component performance. 3.1.4 Selection of specifications and standards. Specifications and standards for necessary commodities and services not specified herein shall be selected in accordance with
16、 MIL-STD-143. 3.2 Materials and processes. The materials and processes used in the manufacturer of components shall conform to the applicable Specifications, in accordance with paragraph entitled “Material Specifications! of ANA Bulletin No. 343 and shall be selected from the list of materials and p
17、ro- -cc cesses apriroWy the procuring activity for the specific application. 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-27420 M 9999906 1341305 564 9 MIL-C-27410 (USAF) 3.2.1 Hetals. Metals shall be compatible vith fluids (3.4.81, fluid
18、vapors, fluid decomposition products, products of combustion where applicable, and with environments to which subjected. In addition, they shall not deteriorate in normal usage and storage. The use of dissimilar metals, especially brass, copper, or steel in contact with aluminum alloy, shall be avoi
19、ded where practicable. Protection of dissimilar metal combinations shall be in accordance with MIL-STD-454 Requirement 16. 3.2.2 Rubbers, plastics, and elastomers. Rubbers, plastics, and elastomers shall be compatible with fluids (3.4.81, fluid vapors, fluid decomposition products, products of combu
20、stion where applicable, and with environments to which subjected. parts shall be in accordance with ANA Bulletin No. 438. Age control of synthetic rubber 3.2.3 Lubricants. Propulsion system components shall not require added lubrication during their normal service life (6.3.11). Ail com- ponent wear
21、 surfaces in contact with system fluids shall not require additional lubrication other than the system fluid itself. Lubricants shall be compatible with fluids. fluid vapors, fluid decomposition products, products of combustion where applicable, and with environments to which subjected. 3.2.4 Finish
22、es. All finishes, surface treatment, plating, coatings, or paints shall be specified in the model specification. 3.3 Performance characteristics. The performance Characteristics, including the intended application and the fluid system interactions, shall be specified in the model specification. as a
23、 minimum. The following shall be included 3.3.1 Operating attitude. Components shall be capable of meeting the performance characteristics specified in the model specification when operated in any attitude the components may be exposed to during their operating life (6.3.6). model specification. The
24、 operating attitudes shall be specified in the 3.3.2 Life characteristics. The component operating and storage life (6,3.12) characteristics shall be specified in the model specifi- cation. 3.3.2.1 Storage life. All rocket fluid system components shall have a minimum required storage life (non-opera
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