AIR FORCE MIL-STD-3035-2013 USAF AIRCRAFT ARRESTING SYSTEMS.pdf

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1、 AMSC N/A FSC 1710 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited INCH-POUND MIL-STD-3035 (USAF) 05 July 2013 DEPARTMENT OF DEFENSE DESIGN CRITERIA STANDARD USAF AIRCRAFT ARRESTING SYSTEMS Provided by IHSNot for ResaleNo reproduction or networking permitted without

2、license from IHS-,-,-MIL-STD-3035 ii FOREWORD 1. This standard is approved for use by the Department of the Air Force and is available for use by all Departments and Agencies of the Department of Defense. 2. This standard is dedicated to land-based aircraft arresting systems (AASs) designed for use

3、with United States Air Force (USAF) tail hook equipped fighter aircraft. 3. Comments, suggestions, or questions on this document should be addressed to AF-99 (agent for AF-84), AFSC/LOEP (WPAFB, OH), 5215 Thurlow St, Bldg 70-C, Suite 5, Wright-Patterson AFB, OH 45433-5750. or emailed to spec99wpafb.

4、af.mil. Since contact information can change, you may want to verify the currency of this address information using the ASSIST Online database at https:/assist.dla.mil/ . Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3035 iii CONTENTS PARAG

5、RAPH PAGE FOREWORD ii 1. SCOPE 1.1. Scope 1 1.2. Classification1 1.2.1. Types 1 2. APPLICABLE DOCUMENTS 2.1. General .1 2.2. Government documents .1 2.2.1. Specifications, standards, and handbooks 1 2.2.2. Other Government documents, drawings, .2 and publications 2.3. Non-Government publications .3

6、2.4. Order of precedence .3 3. DEFINITIONS 3.1. AASs .3 3.2. Operational AASs .4 3.3. Emergency AASs 4 3.4. Energy absorber units (brakes) .4 3.5. Reliability 4 3.6. Functional Span 4 3.7. Split distance .4 3.8. Tape cropping .4 4. GENERAL REQUIREMENTS 4.1. Construction .4 4.2. Design 5 4.3. Configu

7、ration requirements .5 4.4. Purchase tape tensile loading .6 4.5. Off-center arrestments .6 4.6. Material, protective coatings, and finish 6 4.6.1. Recycled, recovered, or environmentally preferable materials .6 4.6.2. Protective coatings .6 4.6.2.1. Surface preparation and pretreatment 6 4.6.2.2. P

8、rimer .6 4.6.2.3. Ferrous surfaces .6 4.6.2.4. Aluminum and mixed aluminum and ferrous surfaces 6 4.6.2.5. Topcoat 7 4.6.3. Dissimilar metals .7 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3035 iv 4.6.4. Drainage .7 4.6.5. Finish7 4.6.6.

9、Fluid traps and fraying surfaces .7 4.6.7. Ventilation7 4.7. Purchase system rewind and tensioning 7 4.8. Safety .8 4.8.1. Component protection 8 4.8.2. System safety .8 4.9. Identification of controls and instruments .8 4.10. Identification of product 8 4.11. Special service tools and kit .8 4.12.

10、Welders and welding8 4.13. Fastening devices .8 4.14. Hydraulic system design 8 4.15. Service life .9 4.16. Reliability .9 4.17. Workmanship .9 4.17.1. Bolted connections .9 4.17.2. Riveted connections .9 5. DETAILED REQUIREMENTS 5.1. Operational AASs 9 5.1.1. Performance .9 5.1.2. Control System.10

11、 5.1.2.1. Programmable aircraft runout 10 5.1.2.2. Data capture .10 5.1.2.3. Diagnostics .11 5.1.2.4. Back-up power .11 5.1.2.5. Shock12 5.1.3. Mobility requirements 12 5.1.3.1. Installation12 5.1.3.1.1. Cruciform stakes 12 5.1.3.2. Tandem towing 12 5.2. Emergency AASs .12 5.2.1. Performance .12 5.3

12、. Packaging .13 6. NOTES 6.1. Intended use .13 6.2. Acquisition requirements .13 6.3. Subject term (key word) listing14 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3035 1 1. SCOPE 1.1 Scope. This standard establishes the minimum military-

13、unique functional requirements for design and development of United States Air Force (USAF) land-based Aircraft Arresting Systems (AASs). 1.2 Classification. AASs are of the following types, as specified (see 6.2). 1.2.1 Types. The types of AASs are as follows: Type I Operational (runway) AASs (see

14、3.2) Type II Emergency (overrun/underrun) AASs (see 3.3) 2. APPLICABLE DOCUMENTS 2.1 General. The documents listed in this section are specified in sections 3, 4, or 5 of this standard. This section does not include documents cited in other sections of this standard or recommended for additional inf

15、ormation or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements of documents cited in sections 3, 4, or 5 of this standard, whether or not they are listed. 2.2 Government documents. 2.2.1 S

16、pecifications, standards, and handbooks. The following specifications, standards, and handbooks form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. FEDERAL STANDARDS FED-STD-595/24052

17、Green, Semigloss DEPARTMENT OF DEFENSE SPECIFICATIONS MILDTL-53030 Primer Coating, Epoxy, Water Reducible, Lead and Chromate Free MILDTL5541 Chemical Conversion Coatings on Aluminum and Aluminum Alloys MIL-PRF-81322 Grease, Aircraft, General Purpose, Wide Temperature Range, NATO code G-395 MIL-PRF-2

18、3377 Primer Coatings: Epoxy, High-Solids MIL-PRF-26915 Primer Coating, for Steel Surfaces MIL-PRF-32014 Grease, Aircraft and Instrument Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3035 2 MIL-PRF-83282 Hydraulic Fluid, Fire Resistant, Synt

19、hetic Hydrocarbon Base, Metric, NATO code H-537 MIL-PRF-85285 Coating: Polyurethane, Aircraft and Support Equipment MIL-W-38461 Webbing, Nylon, Aircraft Arresting (Inactive for New Design) DEPARTMENT OF DEFENSE STANDARDS MIL-STD-130 Identification Marking of U.S. Military Property MIL-STD-810 Enviro

20、nmental Engineering Considerations and Laboratory Tests MIL-STD-882 System Safety MIL-STD-889 Dissimilar Metals (Copies of these documents are available online at https:/assist.dla.mil/quicksearch/ or from the standardization document order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 191

21、11-5094.) 2.2.2 Other Government documents, drawings, and publications. The following other Government documents, drawings, and publications form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or c

22、ontract. NAVAL AIR WARFARE CENTER (CAGE 80020) NAVAIR DRAWING 515053 1 1/4 Dia. Non-rotating Wire Rope (Copies of this document are available from the Naval Air Systems Command, Code 4.1.4, Lakehurst, NJ 08733-5100.) U.S. AIR FORCE (CAGE 98752) USAF DRAWING 66D1751 Connector, 8 1/2-in Tape-BAK-12 Ar

23、resting Barrier, 1 1/4-in Runway Pendant Cable, Assy of USAF DRAWING 7545764 Support, Donut Type-Wire Cable (Copies of these documents are available from Robins AFB GA, (AFLCMC/WNZEC, 460 Richard Ray Blvd Ste 200, Robins AFB, GA 31098-1813) or emailed to 642CBSG.Workflowrobins.af.mil. ) Provided by

24、IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3035 3 2.3 Non-Government publications. The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the

25、solicitation or contract. GULF this includes malfunction or premature function of parts, devices, or mechanisms, which degrade system performance or cause equipment to operate improperly. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3035 5

26、 4.2 Design. AASs shall be based on the split-energy absorber concept (for example, two energy absorber units sited on opposite sides of the runway, working in conjunction to arrest troubled aircraft) with no requirement for mechanical cross-runway interconnection other than the hook cable. The ener

27、gy absorbers shall provide braking force for aircraft weights ranging from 19,000 lbs to 85,000 lbs at velocities up to 200 knots (velocity limited only by the dynamic performance of the hook cable and the kinetic energy capacity of the AAS). This shall be accomplished under a single system setting

28、for the required aircraft weight ranges and engaging speeds herein for example, AASs shall be independent of field level adjustment(s) once programmed for a specific runout distance. The AASs shall be designed for split distance installations up to 300-feet. Further, AASs shall withstand engagements

29、 off-center up to 50 percent of the runway semi-span with no adverse effects to the AAS, to the engaging aircraft, or to the pilot. The AAS shall be designed for: a. concrete pad (for example, above-grade) b. permanent-pit-type (for example, below-grade), and c. when specified by the solicitation, s

30、oil surface (expeditionary) installations. 4.3 Configuration requirements. The energy absorber units of the AAS shall be designed to accommodate the following: a. bidirectional aircraft engagements (for example, engagement by aircraft landing or taking off from the approach or departure runway end),

31、 b. fairlead beams in accordance with CAGE 21439 print number 52-W-2295-201 (NSN 1710-01-098-4984) or equal, c. grease in accordance or compatible with MIL-PRF-81322 or MIL-PRF-32014, d. hook cables in accordance with CAGE 80020 drawing number 515053-90 through 515053-303, e. hook cable support disk

32、s (support disks) in accordance with CAGE 98752 drawing number 7545764, f. hydraulic fluid in accordance or compatible with MIL-PRF-83282, g. purchase tapes in accordance with Type I of MIL-W-38461, and h. purchase element connectors (tape connectors) for connecting the tape to the hook cable in acc

33、ordance with CAGE 98752 drawing number 66D1751. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3035 6 4.4 Purchase tape tensile loading. The purchase tape tensile load imparted by each energy absorber shall not exceed 60 percent of the stren

34、gth of the purchase tape (defined as 63,000 lbs). 4.5 Off-center arrestments and loading. The arrestment loading exerted, by the energy absorbers, from either side of the runway shall be balanced, even in cases of off-centered aircraft engagements. The energy absorbers shall have a moderate tendency

35、 to steer the aircraft toward the midpoint between each energy absorber during runout. 4.6 Materials, protective coatings, and finish. 4.6.1 Recycled, recovered, or environmentally preferable materials. Recycled, recovered, or environmentally preferable materials should be used to the maximum extent

36、 possible, provided that the material meets or exceeds the operational and maintenance requirements, and promotes economically advantageous life cycle costs. 4.6.2 Protective coatings. Materials that deteriorate when exposed to sunlight, weather, or operational conditions normally encountered during

37、 the service life of the item shall not be used or shall have means of protection against such deterioration that does not prevent compliance with the performance requirements specified herein. Protective coatings that chip, crack, or scale with age or extremes of climatic conditions or when exposed

38、 to heat shall not be used. Fasteners, handles, and fittings used in the assembly of the item shall also be primed and painted. 4.6.2.1 Surface preparation and pretreatment. Surface preparation and pretreatment shall be in accordance with the respective primer and topcoat specifications. Structures

39、shall be cleaned and degreased and scuffed or blasted prior to priming; primer shall be applied before any oxidation or rusting occurs. Aluminum surfaces shall have MIL-DTL-81706, Type II, Class 1A, and MIL-DTL-5541, Type II, Class 1A, chemical conversion coating applied in accordance with the manuf

40、acturers directions prior to priming. 4.6.2.2 Primer. Raw metal edges, to include fastener and drain holes, with exception to any non-ferrous metals such as stainless steel or aluminum hose ends, bolts, washers and nuts, shall be coated with primer before applying topcoat. 4.6.2.3 Ferrous surfaces.

41、Ferrous structures and surfaces shall be primed with a water reducible zinc rich primer in accordance with MIL-PRF-26915, Type II, Class B; this shall be followed, within four hours, by a coat of MIL-DTL-0053030 intermediate primer in a wet-to-wet primer application. This two part primer system shal

42、l yield a dry-film thickness of 2.0-2.5 mils for the zinc primer and 0.9 to 1.1 mils for the intermediate primer. The two-primer system shall be allowed to dry and fully cure in accordance with the primer manufacturers directions prior to top coating. 4.6.2.4 Aluminum and mixed aluminum and ferrous

43、surfaces. Aluminum and mixed aluminum and ferrous structures and surfaces shall be primed with an epoxy primer, Type Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-3035 7 II, Class N of MIL-PRF-23377. This single part primer system shall yie

44、ld a dry-film thickness of 0.6 to 0.8 mils. 4.6.2.5 Topcoat. Topcoat shall be polyurethane in accordance with Type I, Class H of MIL-PRF-85285. Neither Chemical Agent Resistant Coating (CARC) nor powder coating shall be used. Topcoat shall be applied to a dry film thickness of 1.6 to 2.4 mils in all

45、 instances, regardless of the primer system utilized. The coating shall be free from runs, sags, orange peel, or other defects. 4.6.3 Dissimilar metals. Use of dissimilar metals as defined by MILSTD889, in contact shall be limited to applications where similar metals cannot be used due to peculiar d

46、esign requirements. When it is necessary to use dissimilar metals in contact, the metals shall be protected against galvanic corrosion. Galvanic corrosion can be minimized by interposition of a material which will reduce the overall electrochemical potential of the joint or by interposition of an in

47、sulating or corrosion inhibiting material such as sealants and organic coatings. 4.6.4 Drainage. Drain holes shall be provided to prevent collection or entrapment of water or other unwanted fluid in areas where exclusion is impractical. All designs shall include considerations for the prevention of

48、water or fluid entrapment and ensure that drain holes are located to effect maximum drainage of accumulated fluids. The number and location of drain holes shall be sufficient to permit drainage of all fluids when the unit is in a 10 degree incline in any plane. The minimum size of the drain holes shall be 0.25 inch. 4.6.5 Finish. The exterior finish color of the AAS shall be color 24052 in accordance with FED-STD-595. 4.6.6 Fluid traps and faying surfaces. There shall be no fluid traps on the AAS. Faying surfaces of all structu