AIR FORCE MIL-P-83126 A-1980 PROPULSION SYSTEMS AIRCREW ESCAPE DESIGN SPECIFICATION FOR《空勤人员逃生用动力装置的设计规定》.pdf

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1、Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-8312bA 13 779770b 03b2877 O W MIL-P-83126A 2.1 Issues of documents. The following documents of the issue in effect on date of invitation for bids or request for proposal, form a part of the specif

2、ication to the extent specified herein. SPEICIFICATIONS - FEDERAL TI-E-516 PPP-B-621 PPP-T-66 MILITARY MIL-P-116 poD.D-lOO0 MIL-S-5002 MIL contractor shall prepare a detailed FMEA using MIL-SW2067 as a guide and shall suhit it to the GPA for approval. 3.2.28 ccxnponent compci tibiity tests. ,mS ccan

3、ponent ccmpatibility tests shall be perfomaed by the contractor during Phase I unless already available) to determine the effects of interaction mng propellant ingredients, propllant liner, propllant ignition material, and other ingrdients such as adhesives, lubricants, etc. include, but not be limi

4、ted to, differential theml analysis and accelerated ageing studies. the age life of the WS will not be reduced below 7 years because of inccpnpatibilities with the AEPS. The GPA reserves the right to require and perform tests on any chdcals, materials, or canbinations which, in its opinion, my degra

5、de with age. During final stage of Phase 1 and prior to the beginning of Phase II, the contractor shall mufacture .and culmit a full scale cut-away model of the design unit to the A. ccpnponentc shall be replace with inert mterial in the sam configuration as the explosive ccanponents. to reveal crit

6、ical internai canpnents and maximize the information obtained fran thermdel. These tests shall These tests shall demonstrate to the BA that 3.2.29 Cut-away model. The explosive The location of the cut shall be selected 24 Provided by IHSNot for ResaleNo reproduction or networking permitted without l

7、icense from IHS-,-,-a P a MIL-P-8312 6A 3.3 Phase II (design verification! . the contractor shall meet the following: Prior to beginning Phase II, a. Al1 requiremats of Phase I shall have been perfomied and approved by the GPA. b. A cut-away model shall be available for review. c. Ail Phase I data s

8、hall be suirnitted. d. A preliminary design review of the current configuration shall be performad (see 3.6.5.1.). 3.3.1 Design verification test sanple.Fourteen loaded AEPS, five of each igniter assembly, and 10 one-gallon blocks of propellant shall be suhnittedto the Naval Ordnance Station, Indian

9、 Head, MD design verification tests of TABI;E: III (see 3.8). assa&y/subassanb1y/mhponent to meet ail applicable requirementc shall be cause for imrsdiate Suspension of the test prqram. At the option of the GPA, the preliminary design review of 3.3.d shall be reconvened to detemne/agree upon future

10、actions to be taken prior to test continuance. Restart Will occur only after approval of the failure analyses and corrective action plan by the BA. (WIH) for Failure of any 3.4 Phase 111 (service release test). Before begnnng Phase III, the contractor shall met the following: a. Al1 requirements of

11、Phase II shall have been performed and approvd by the GPA. b. An updated cut-away model of 3.3.b shall be available for review. c. Al1 Phase I and IT data shall have been suhitted. d. A critical design review of the configuration 3.4.1 Phase III test sanples. The test swle sha fornial documentation

12、and all data shall be performed in 3.4.1.1 and 3.4.1.2. identification see 3.6.5.21. 1 be as defined 3.4.1.1 Service release cmpnent test sample. A test sanpie consisting of 82 loaded AEPS, tw nert AEPS, tw one-gallon blocks of cured propellant (equally divided between at least tm batches) for each

13、propellant type used in the AEPS, and the required propulsion unit information shall be delivered to NOCM for servce release testing (see 3.8). The service release test sample units shall be manufactured to the design established by the critical design review and approve3 by the GPA. It shall be man

14、ufactured with the same equipent, environnent and procedures as proposed for production units. 25 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-t MIL-P-83L26A 13 7979706 0362703 4 TABLE III. Design Verification Test Program. SECTION Igniter to Pmax

15、 dosed bomb at -65OF 123 4 5 26 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-83L2bA 13 7777706 0362704 6 MIIrP-83126A 3.4.1.1.1 Service release test. The sample of 3.4.1.1 shall be tested in accordance with TABLE IV. Failure of any assembly/

16、subassembly to nieet a1 applicable requirerents shall be cause for irrpnediate suspension of the test program. At the option of the GPA the critical review of 3.4d shall be reconvened to detemne/agree upn future actions to be taken prior to test continuance. analysis and corrective action plan by th

17、e BA. 3.4.1.1.2 -life study. Eighteen loaded AEE3 frm the service release test sqle (equally divided between propellant batches) shall be designated for type-life study (accelerated aging). The units shall be retained by the carripletion of service release testing, the units shall be delivered to th

18、e Naval Ordnance Station, Indian Head, M (Me 3012). Tests conducted with typelife units shall not be applied to acceptability of the AEPS as deter- Restart will occur only after approval of the failure . contractor until carpletion of the service release test program. FollaJincJ - mined during servi

19、ce release testing. 3.4.1.2 AES (Aircrew Escape System) system and subsystem test sample. For units that are manufactured for AES system/subsystem testing, the acceptance test sample size submitted to NS/IH shall be in accordance with MuiSW414, inspection level III, for each temperature tested balli

20、stic data shall be analyzed and the lot accepted in accordance with MIL-SI!-414, standard deviation method, single or double specification lMt (as applicable), variability unknm with an AQL of 2.5 percent. requirerents shall be satisfied for all phases of the contract. such as prhers, ignition mater

21、ials, cartridges, initiators, and iters which were mufacture 12 or mre mnths prior to the contract date shall not be used. The propellant cartridge and rocketmtor shall not be manu- factured prior to 150 days before the original contract Lieduled delivery date for the applicable,phase acceptance tes

22、t units. The 3.5 Caeral requirements. Unless otherwise specified, the following 3.5.1 Life. All explosive components except propellant used in the AES, - 3.5.1.1 Priniers. Except as otherwise specified, primers for contract requirenients will be supplied as mlby Naval Ordnance Station, Indian Head,

23、M. Prbrs will be supplied for proprietary items only on an exception basis, when use of GEM is determined, by the CFA, to be to the Governments advantage. Where prhrs are not supplied as GFM, the primers shall meet the life require- ments of 3.5.1 and all applicable Government or c-rcial specificati

24、on re- quirements for the primer. reliability dud test as follows: Additionally, the lot shall be subjected to a (a) A sample of 2300 primrs frm the lot shall be functionally tested at the minimum all-fire energy established by the primer specification. A ball drop test fixture shall be used for the

25、 test. shall be tested in cases or a die which reasonably simulates end item conditions (e.g., pocket diameter, primer reconsolidation). The primers 27 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-8312bA 13 = 0b 03b2705 8 i! f. 28 Provided b

26、y IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-P-8 3126A E 29 I Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NIL-P-83L2bA 13 m 77777Ob 03b2707 L m I 30 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-