1、MIL-T-6010lA(KU) I( * 0 I 15 18 July 1974 SUPERSEDING MIL-T-60101 (MU) 24 January 1964 MILITARY SPECIFICATION THRUSTER, CARTRIDGE ACTUATED, M9 ASSEMBLY This specification is approved for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 This specification covers the Thru
2、ster, Cartridge Actuated, M9, Assembly loaded with Cartridge, Impulse, Mi19 for use in conjunction with other propellant actuated devices in aircrew emergency escape systems. 2. APPLICABLE DOCUMENTS 2.1 The following documents of the issue in effect on date of invitation for bids or request for prop
3、osals, form a part of this specification to the extent specified herein, SPECIFICATIONS Military MIL-A-2550 MIL-P-19834 - Ammunition and Special Weapons, General Specification - Plates, Identification, Metal Foil, Adhesive For Backed STANDARDS Military MIL-STD-105 MIL-STD-109 PIS 28 74 1 - Sampling
4、Procedures and Tables for Inspection by - Quality Assurance Terms and Definitions - Hose Assembly Detachable End Fitting, Medium Attributes Pressure DRAWINGS Armament Command F10520478 Ca845196 - Thruster, Cartridge Actuated, M9 Assembly - Box, Fiberboard (Inner) Packing Ammunition for Thruster, CIA
5、 M9 FSC 1377 THIS DOCUMENT CONTAINS /o PAGES. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-bOLOLA L3 79999Ob 0335583 9 MIL-T-6010lA(MU) 2.1 (Contd) DRAWINGS (Cont d) C8845197 - Box, Packing, Ammunition for Thruster, Cartridge C9217287 - Box,
6、 Fiberboard (Outer) Alternative Packing, IEL-10520478 - Inspection Equipment List for Thruster, Cartridge Actuated M9 Ammunition for Thruster CIA, M9 Actuated , M9 Assembly (Copies of specifications, standards, and drawings required by suppliers in connection with specific procurement functions shal
7、l be obtained from the procuring activity or as directed by the Contracting officer.) 3. REQUIREMENTS 3.1 General.-Material, parts and assemblies shall comply with the requirements specified in the applicable drawings and specifications. 3.2 Torque.-Torque requirements shall be as specified in Table
8、 I. No move- ment shall occur upon application of the breakaway torque. TABLE I Component A B Seating or Bottoming Breakaway (inch pounds) (inch pounds) Breech 4.2.2 Examination.-One-hundred percent examination shall be performed for all critical defects. for all critical defects. on a defect basis
9、in accordance with the classification of defects contained herein, using the sampling plan and associated criteria in Table II. allowable defects per class for either the major or minor classification shall not exceed the acceptance number of Table II. rejected. ation for such defects as burr and fo
10、reign matter. Examination for major and minor defects shal1,be performed Examination for major and minor defects shall be performed The total number of All nonconforming materials shall be Four power (4X) magnification may be used in performing visual examin- TABLE II Minor Lot Size Sample Size Ma j
11、 or Accept Reject Accept Reject 1 - 300 100% Examination 301 - 800 50 O 1 1 2 801 - 1800 90 1 2 2 3 4.2.2.1 Cartridge, Impulse N119, Drawing D8595513, covering a detail of Drawing F10520478. Defect Method of Inspection CRITICAL 1. Mixed cartridges Visual 2. Metal defective Visual 3. Marking missing,
12、 incorrect or illegible Visual 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-6010lA(MU) 4.2.2.1 (Contd) Defect MAJOR Method of Inspection 101. Foreign matter MINOR Visual 201. Case scratched or dented Visual 4.2.2.2 Breech and FirinF Pin, S
13、ub-assembly consists of: Breech 10520483, Firing Pin 10520485, “O“ Ring 1.12828775-909 covering a detail of Drawing F10520478. CRITICAL 1. Firing pin hole obstructed MAJOR Visual 101, Thread damaged or not full Visual 102. Protective finish inadequate or defective Visual 103. Burr Visual 104. Foreig
14、n matter Visual MINOR None defined 4.2.2.3 Assembly Drawing F10520478 less Trunnion 10520490 Collar 10520484 and %ping Plug 8593299. CRITICAL 1. MAJOR Head of breech in contact with body 101. Excess sealant not removed 102. Thread damaged or not full 103. Burr 104. Foreign matter MINOR 201. Protecti
15、ve finish inadequate or defective 5 Visual Visual Visual Visual Visual Visual Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Defect CRITICAL 1. Shear pin not enga d in firing MAJOR in 101. 102. Total length 103. Thread damaged 104. Total length from
16、 center of trunnion to face of adapter Foreign matter in gas port MINOR None defined 4.2.2.5 Assembly, Drawing F10520478. - CRITICAL 1. Any part missing, except as defined below 2. Improper assembly, except as otherwise classified 3. Shear pin missing in shear ring 4. Cartridge missing 5. Metal defe
17、ctive 6. Marking missing, incorrect or illegible MAJOR 101. Trunnion not free to rotate 360 degrees 102. Breech above flush 103. Threads damaged or not full MINOR 201. Total length max. 202. Protective finish defective 203. 204. Location of labels, incorrect Shipping cap or plug missing 6 Gage Gage
18、Visual Visual Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-60101A 13 m 7979906 O335588 8 mi MIt-T-6010lA(MU) 4.2.2.6 Box, Fiberboard (Inner) Drawing C8845196 Defect Method of Inspection CRITICAL None defined MAJOR None defined MINOR 201. Con
19、tents loose -202. Box broken or damaged 203. 204. 205. Number of units contained incorrect Marking missing, incorrect or illegible Tape incomplete or badly wrinkled Manual Visual Visual Visual Visual 4.2.2.7 Box, Packing Drawing C8845197 CRITICAL None defined MAJOR None defined MINOR 201. Contents l
20、oose Manual 202. 203. Contents of box exposed Visual 204. Box damaged Visual 205. Marking misleading or unidentifiable Visual 206. Number of units incorrect Visual Strapping missing, loose, broken or improperly assembled ?lanual/Visual 4.2.2.8 Box, Fiberboard (Outer) Alternative Packing Ammunition,
21、Drawing C9217287. CRITICAL None defined MAJOR None defined 7 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- _ _ MIL-T-60LOLA 13 9797706 0335587 T MIL-TdOlOU (MU) 4.2.2.8 (contd) Defect Method of Inspection MINOR 201. Contents loose tanual/Visual I
22、202. Carton broken or damaged Visual 203. Number of units incorrect Visual 204. Marking missing, incorrect or illegible Visual 205. Tape incomplete Visual 4. ,3 Inspection testing.ghe following tests shall be performed in accorda with 4.3. 4.2.3.1 Breakaway torque. 4.2.3.1.1 Breech and body.-Each br
23、eech and body sub-assembly shall be subjected to a breakaway torque application. ments of 3.2 shall be cause for rejection of the sub-assembly. Failure of any unit to comply with the require- - 4.2.3.1.2 Breech and collar.-Each breech and collar of the thruster assembly shall be subjected to a break
24、away torque application. comply with the requirements of 3.2 shall be cause for rejection of the thruster. Failure of any unit to 4.2.3.2 Residual magnetism.-Each thruster assembly shall be tested for excessive residual magnetism. ments of 3.4 shall be cause for rejection of the assembly. Failure of
25、 any thruster to comply with the require- 4.2.3.3 Functional tests,-The following tests shall be performed by the Government. 4.2.3.3.1 Ballistics.-Units shall be tested to determine compliance with the requirements of 3.5.1 and 3.5.8. provided in Table IIIand 4.3.4.1.1. Failure of any unit to compl
26、y with the require- ments shall be cause for rejection of the lot. The unit shall be temperature conditioned as TABLE III Temperature Sample Size Method -65 degrees to -70 degrees F 7 200 degrees to 205 degrees F 7 Load Load 4.2.4 Inspection equipment.-The examination and tests shall be made using t
27、he equipment listed on IEL 10520478. 8 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-4.3 Test methods and procedures. 4.3.1 Breakaway torque. 4.3.1.1 Breech and body.-The breakaway torque shall be applied to the breech after insertion of cartridge
28、and the thread sealing compound has been cured in accordance with the drawing requirement. An air rise or other holding fixture shall be used to secure the body. 4.3.1.2 Breech and collar.-The breakaway torque shall be applied to the collar after the thread sealing compound has been cured in accorda
29、nce with the drawing requirement. 4.3.2 Residual magnetism.-The thruster shall be tested or excessive residual magnetism in an area free of local magnetic effects by placing the thruster 6 inches from andat the same height as the compass, in a north-south horizontal position with the compass set in
30、an east-west heading, The thruster shall be moved slowly pass the compass in a longitudinal direction for its entire length, rotated 90 degrees in the horizontal position about ies longitudinal axis and moved slowly back past the compass. 90 degree rotation of the thruster around its longitudinal ax
31、is. This procedure shall be repeated for each 4.3.4 Functional. 4.3.4.1 Ballistics.-The test samples shall be rigidly supported so that the entire thrust is borne by the thruster mounting points. tested within 10 minutes after removal from the temperature conditioning chamber, When this time limit i
32、s exceeded, the sample units shall be reconditioned at the original temperatures. The-samples shall be 4.3.4.1.1- Temperature conditioning. - A simulated thruster and cartridge with a temperature sensitive element, placed in the dmy cartridge, shall be stored in a temperature conditioning chamber at
33、 he same time as the samples. conditioning time shall be a minimum of one hour longer than the time necessary for the temperature of the simulated cartridge to reach the required test temperature. The temperature 4.3.5 X-ray.-The equipment and procedure specified herein shall be used to perform the
34、x-ray examination. 60 seconds. A high intensity viewer shall be used to determine deflectiveness of units, 5. PREPARATION FOR DELIVERY The equipment shall be 80 Kilovolts, 10 milliamperes, The target to film distance shall be 36 inches, minimum, using AA film. 5.1 Packing and marking.-Packing and ma
35、rking shaIl be as specified by the procuring activity: Level B - In accordance with drawings C8845196 and C9217287. Level A - In accordance with drawings C8845196 and C8845197; 9 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-60101A 13 777770b
36、 0335571 A W MIL T-6010lA(MLl) 6. NOTES 6.1 A mechanical failure is defined as any deformation or breakage of a part, the occurrence of which .is other than a design function. 6.2 those existing in aircraft shall be referred to as load condition in this specifi- cation. U.-The expected performance o
37、f the thruster under conditions simulating 6.3 Ignition delay is defined as the time lapse between the firing of the cartridge and the beginning of the continuous pressure rise in the body of the thruster, 6.4 Explosive Hazard Classification Information: Explosive Hazard Class - 1 Storage Compatibil
38、ity Group - B, E, N DOT Hazard Class - C DOT Marking - Explosive Power Device, Class C Handle Carefully - Keep Fire Away 6.5 Hazard notice,-The thruster described herein and certain of its components are flammable and/or explosive, consequently presents hazards in manufacture, handling, storage and
39、shipments. The contractor should recognize these hazards to take appropriate measures to guard and protect against fire, explosion, adverse environment, corrosive atmosphere, rough handling and electrically induced incidents. 6.6 Ordering data.-Procurement documents should specify the title, number and date of this specification. Custodian : Army - MU Preparing activity: Amy - MU Project No. 1377-A584 * U. s. GOVERNMENT PRINTING OFFICE 1974-603- 109/854 10 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
