NAVY MIL-C-82734 A-1988 CATAPULT AIRCRAFT EJECTION SEAT CKU-5 A A ASSEMBLY《CKU-5 A A型飞机弹射座椅弹射器组件》.pdf

1、MIL-C-82i34A 13 W 3999906 03b2750 5 C-/!- 03 I INCH-POUND I MlL-C-82734A(OS 27 October 19 R 8 SUPERSEDING 28 February 1984 MI L-C-82734(OS) MILITARY SPECIFICATION CATAPULT, AIRCRAFT EJECTION SEAT CKU-SINA ASSEMBLY This specification is approved for use within the Naval Sea Systems Command, Departmen

2、t of the Naw, and is available for use by all Departments and Agencies of the Department of Defense. i. SCOPE 1.1 Scope. This specification covers the minimum requirements for the procurement of the Rocket Catapult CKU-5INA loaded assembly. 2. APPLICABLE DOCUMENTS 2.1 Government documents. 2.1.1 Spe

3、cifications and standards. The following specifications and standards form a part of this specification to the extent specified herein. Unless otherwise specified, the issues of these documents shall be those listed in the issue of the Department of Defense Index of Specifications and Standards (DoD

4、ISS) and supplement thereto, cited in the solicitation. SPECIFICATIONS MILITARY M IL-P-116 Preservation, Methods of MIL-I-6868 Inspection Process, Magnetic Particle MIL-S-9479 MlL-P-82663 Propellant, Solid, Composite Seat System, Upward Ejection, Aircraft, General Specification for STANDARDS MILITAR

5、Y MIL-STD-105 Sampling Procedures and Tables for Inspection by Attributes MIL-STD-129 Marking for Shipment and Storage MlL-STD-414 Sampling Procedures for Inspection by Variables for Percent Defective MIL-STD-453 Inspection, Radiographic Beneficial comments (recommendations, additions, deletions) an

6、d any pertinent data which may be of use in improving this document should be addressed to: Commanding Officer, Naval Ordnance Station, Standardization Branch (3730), Indian Head, MD 20640-5000, by using the self-addressed Standardization Document Improvement Proposai (DD Form 426) appearing at the

7、end of this document or by letter. AMSC NO. N4546 FSC 1377 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. - , . THIS DOCUMENT CONTAINS /?5 PAGES. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-, MIL-C-8273VA 13 m 7

8、77770b 0362751 7 I M lL-C-82734A(OS) 8 MlL-STD-810 Environmental Test Methods and Engineering Guidelines MIL-STD-1168 Ammunition Lot Numbering M IL-STD-21 O1 Classification of Characteristics MS 17983 Compass, Magnetic, Pilots Standby 2.1.2 Other Government documents, drawings and publications The f

9、ollwing other Government documents, drawings, and publications form a part of this specification to the extent specified herein. Unless othennrise specified, the issues shall be those in effect on the date of the solicitation. CODE OF FEDERAL REGUUTIONS 49 CFR 100-199 Transportation DRAWINGS NAVAL S

10、EA SYSTEMS COMMAND (CAGE Code 53711) DE184322 List of Drawings, Catapult, Aircraft Ejections Seat, CKU-5IAIA Assembly (Copies of specifications, standards, drawings, and other Government documents required by contractors in connection with specific acquisition functions should be obtained from the c

11、ontracting 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 specified, the issues of the documents which are DoD adopted shall be those listed in the issue of the Do

12、DISS specified in the solicitation. Unless othewise specified, the issues of documents not listed in the DoDISS shall be the issue of the nongovernment documents which is current on the date of the solicitation. AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) E-165-80 Liquid Penetration Inspection

13、 Method (Application for copies should be addressed to the American Society for Testing and Materials, 1916 Race Street, Philadelphia, PA 19108) NATIONAL MOTOR FREIGHT TRAFFIC ASSOCIATION, INC., AGENT National Motor Freight Classification (Application for copies should be addressed to the National M

14、otor Freight Traffic Association, Inc., ATA TRAFFIC Dept, 2200 Mill Road, Alexandria, VA 22314.) UNIFORM CLASSIFICATION COMMITTEE, AGENT Uniform Freight Classification (Application for copies should be addressed to the Uniform Classification Committee Agent, Tariff Publication Officer, Room 1106, 22

15、2 South Riverside Plaza, Chicago, IL 60606.) (Nongovernment standards and other publications are normally available from the organizations which prepare or distribute the documents. These documents also may be available in libraries or other informational services.) 2 i Provided by IHSNot for Resale

16、No reproduction or networking permitted without license from IHS-,-,-r- O MIL-C-8273VA 13 = 7779906 0362752 7 I MI L-C-82734A(OS) 2.3 Order of precedence. In the event of a conflict beween the text of this specification and the references cited herein, the text of this specification shall tala prece

17、dence. Nothing in this specifiction, however, shall supersede applicable laws and regulations unless a specific exemption Ras been obtained. 3. REQUIREMENTS 3.1 First Article. Unless otherwise specified in the contract or order (see 82.1), first article samples of the catapult assemblies are require

18、d and shall be manufactured using the methods and procedures proposed for production. The samples shall be tested as specified in section 4 for the purpose of determining, prior to starting production, that the contractors production methods are capable of praducing catapult assemblies that comply w

19、ith the technical requirements of the contract (see 4.4). 3.1.1 Pressure transduce=. All first article samples catapult assemblies shall be adapted for pressure transducers as specified in the contract or order (see 6.2.1 and 65). 3.1.2 Propellant aging. Propellant samples shall be prepared and test

20、ed in accordance with the requirements of 4.4.3. Tests will be performed in accordance with MIL-P-82663. Failure of the propellant to meet the requirements of MIL-P-82663 will be cause for rejection of the batch. 3.2 Materials. All materials, parts, and assemblies shall be in accordance with the DL

21、5184322, this specification, and the documents referenced herein. 3.2.1 Primary Components. Only primary Components from a single primary component lot shall be used in a production lot of loaded rocket catapults. 3.2.2 Propellant. The propellant shall be in accordance with Mli-P-82663. 3.3 Age. 3.3

22、.1 Explosive components. All primeffi shall have been manufactured and certified within 24 months or recertified within 12 months of the assembly date of the catapult assembly lot. All other explosive components including but not limited to igniteffi, shall have been manufactured or recertified with

23、in 12 months of the assembly date for the rocket catapult assembly lot. - 3.3.2 Propellant. The propellant shall be manufactured within the 150 days prior to the assembly date for the rocket catapult assembly lot. 3.4 Performance and product characteristics. The rocket catapults shall meet the follo

24、wing performance and product characteristics when test fired at -65, +70, and +165 OF using an ejected weight of 375 pounds. 3-4.1 Ballistic. The rocket catapults shall meet the ballistic performance parameters specified in table I. 3 Provided by IHSNot for ResaleNo reproduction or networking permit

25、ted without license from IHS-,-,-MIL-C-273+A i13 m 777770b 03b2753 O W -65 OF MIIJ I MAX Parameter MIL-C-82734A(OS) 70 OF 165 OF MIN MAX MIN MAX AQL TABLE I. Ballistic performance requirements (375 pound ejected weight). 400 35 - - 600 22.0 30 - Initiation pressure si) and that the disposal of any t

26、ested hardware, propellant, or metal parts without authorization by the contracting activity will result in the test being declared invalid, and a retest will be required. 6.9 Retention of radiographs. All radiographs of accepted lots of rocket catapults are to be retained on file by the contractor

27、for 9 years or 1 year past the service life of the unit, whichever is longer. 14 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-82734A 13 m 7779906 03627bLi 5 m -L MI L-C-82734A(OS) 1 6.10 Life. The rocket catapult has a design life of 8 years

28、 with an installed service life of 8 years from the date of propellant manufacture. 6.11 Changes from previous issue. Asterisks are not used in this revision to identify changes with respect to the previous issue due to the extensiveness of the changes. 6.12 Subject terms (keyword) listing. Ejection equipment, aircraft Propellant Propellant actuated device Safety equipment, aircrew Preparing Activity Navy - OS (Project 1377-N931) &US. GOWRNMENT PRINTING OFFICE: 1989 - 604433/I709 os Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-