ARMY DOD-P-63986-1982 PELLET FLASH TUBE 1B52《1B52型闪光管用弹丸》.pdf
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1、DOD-P-63986 (AR) 14 MY 1982 MILITARY SPECIFCATION Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improvin this document should be addremed to: Commander, US Army Armament however, the standard deviation requirement shall be met. Velocity dat
2、a shall be corrected to the muzzle condition using a positive correction value of +0.75 m/sec per meter multiplied by the distance between the muzzle and the midpoint of the velocity screens. See 6.3.1 for example of this procedure. 4.5.4.10 Action time. The test rounds shall be conditioned at -54OC
3、, 21C and 71C and fired from a test fixture barrel. The time between application of voltage to primer and exit of the projectile from the muzzle shall be measured. The time shall comply with the requirement of Table I. Any corrected action time of 2.40 milliseconds or less shall be regarded as a pot
4、ential instrumentation error and referred to the Government for disposition. 17 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-DOD-P-b37b 13 I 7777906 0352500 7 m DD-P-63986 (AR) 4.5.4.11 Environmental tests. Unless otherwise pecified, performance d
5、uring and/or after environmental exposure, as specified in the applicable test procedure, shall consist of conducting the tests of 4.5.4.8, 4.5.4.9 and 4.5.4.10. except all test rounds shall be conditioned at 21OC prior to firing. -. , 4.5.4.11.1 Temperature, humidity and altitude. The test rounds s
6、hall be subjected to the temPerature/humiditv/altitude test f MIL-STD-810; Method 504. shall be examined for deterioration and subjected to the test referenced in 4.6.2. Afier exposure, th test item 4.5.4.11.2 Aircraft vibration. The test rounds shall be subjected to a broad band random vibration pr
7、ofile in accordance with the requirements of MIL-STD-810, Method 514.2, Procedure I, Category C, except the vibration spectrum shall be as shown in Figure 1. The test item shall be mounted to a test fixture simulating an AAH magazine in a normal airplane mounting as specified by the procuring agency
8、. The test duration shall be 45 minutes in each of three mutually perpendicular axes at each of two temperature conditions, -40 +2.BoC and 65.5O +2.8OC. Following exposure, all of the test items shall be-subjected to the tests referenced in 4.3.2. 18 I Provided by IHSNot for ResaleNo reproduction or
9、 networking permitted without license from IHS-,-,-DOD-P-b39Bb 13 I 977770b 0352503 O W DOD-P-63986 (AR) 2000 1000 500 100 n 50 10 5 1 TIME (MINUTES) FIGURF, I. VIBRATION TEST REQUIREMENTS 19 i: I. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- i -
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