MIL-HDBK-244A 6 apr 90.pdf

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MIL-HDBK-244A ‘1 CONTENTS PARAGRAPH 5.3.1 5.3.2 5.3.3 5.3.4 5.3.5 5.3.6 5.3.6.1 5.3.6.1.1 5.3.6.1.2 5.3.6.1.3 5.3.7 5.3.7.1 5.3.7.2 5.3.7..2.1 5.3.7.2.2 5.3.7.2.3 5.3.7.3 5.3.7.3.1 5.3.7.3.2 .5.3.8 5.3.9 5.3..9,1 5.3.9.2 5.3.9.3 5.3.9.4 5.3.9.5 5.3.10 5.3.10.1 5.3.10.2 5.3.10.3 5.3.10.4 5.3.10.5 5.3.10.6 5.3.10.7 5.3.11 5.3.11.1 5.3.11.1.1 5.3.11.2 5.3.11.3 5.3.11.4 “5.3.11.5 5.3.12 5.3.12.1 5.3.12.2 Design parameters.................................... Release conditi.ons................................... Carriage environment................................. Droppable stores..................................... Aircraft pyrotechnic equipment.................. ..... Classes of airborne stores’........................... Dispensers,........................................... Class 2 dispensers................................... Dispensing operation................................. Dispenser jettison................................... Store aerodynamics....*.............................. Trade offs.......~.................................... Drag................................................. PAGE 72 Free-bodydrag...............................-:..-.-...”.-. .-. 72 Installation factor.................................. Supersonic..............................“............ Stability............................................ Destabilizing effects................................ Stability factors for various store classes......... Analysis of store clearances and.fit................. Store electrical ....................... interface...● Store electrical connectors.......................... Store pin function assignments...................*... Connector location........*.......................... Store power requirements...“..............“........... Connector keyway..................................... Store mechanical interface”........................... Store mechanical interference........................ ‘!All-up”delivery ~o aircraft...:.................... Store lugs,........................................... Sway brace compatibility............................. Ejector areas................................*....... Weight and”centerof gravity.......................... Special equipment and services....................... Store structural requirements..............-o........ Store/aircraft structural interface.................. Deformation at interface............................. Carriage loads irnposedon store...................... Store flutter and vibration.......................... Store dynamic response............’..........’........ Landing loads imposedon store...................... Store environment.................... ............... Store aeroacoustic parameters........................ Store thermal environment............................ 68 69 69 69 _. 69 69 70 70 71 71 71 71 72 72 72 72 73 75 75 75 76 76 77 77 77 77 78 78 78 78 78 79 “ 79 79 79 79 80 80 80 80 81 81 . . . Vlll ,, Source: http://www.assistdocs.com -- Downloaded: 2009-07-16T13:55Z Check the source to verify that this is the current version before use.
MIL-HDBK-244A CONTENTS PARAGRAPH 5.3.12.3 5.3.12.4 5.3.12.4.1 5.3.12.4.2 5.3.12.4.3 5.3.12.4.4 5.3.12.4.5 5.3.12.4.6 5.3.12.4.7 5.3.13 5.3.13.1 5.3.13.1.1 5.3.13.1.2 5.3.13.1.3 5.3.13.1.4 5.3.13.1.5 5.3.13.1.6 5.3.13.1”.7 5.3.13.1.8 5.3.13.1.9 5.3.13.1.10 5.3.13.1.11 5.3.14 5.3.14.1 5.3.14.1.1 5.3.14.1.2 5.3.14.1.3 5.3.14.1.4 5.3.15 5.3.15.1 5.3.16 5.3.16.1 5.3.17 5.3.17.1 5.4 5.4.1 5.4.2 5.4.2.1 5.4.2.2 5.4.2.3 5.4.2.4 5.4.3 5.4.4 5.4.5 5.5 Operational vibration................................ - -, ., . . . . . brore electromagneticcrlterla....................... Store electroexplosivesubsystems.................... Store electromagneticinterference................... Store electrical bonding and lightning protection.... Store engine electrostaticcharging.................. Store electrostaticprotection....................... Store EMI filters.................................... Store electromagneticenvironment.................... Loading and handling.................................. Stores design as a function of AGE and GSE requirements Packaging............................................ Transportation........................’.............. Assembly............................................. Cradle area..........................’................... Strongback and sway brace areas...................... Hoist band areas..................................... External protuberances............................... Flight line assembly or removal...................... Special tool requirements............................ Markings............................................. Adapter cables and store suspension requirements..... Fuzing and arming..................● ..● .............. Fuze and weapon...................................... Mechanical fuze connections.........................’. Mechanical fuze characteristick...................... Electrical fuze connectionsand characteristics...... Digital fuzing....................................... Reliability and maintainability...................... ,Storesystem effectiveness........................... Mass properties variation............................ Mass properties tolerances........................... Conflagration........................................ Store fire protection................................ Stores management system............................. Stores management equipment........................... SMS electrical interfaces............................ Electrical connectors................................ Pin function assignments............................. Location of electrical connectors.................... Electrical input power............................... SMS mechanical interface.............................. Controls and displays................................ General design criteria.............................. Helicopter application............................... ~ 81 81 82 82 82 . 82 ‘- 82 82 :: :: 83 83 83 83 83 84 84 84 84 84 84 84 84 85 85 85 86 86 86 86 86 87 87 87 87 88 88 89 89 89 89 ;: ix Source: http://www.assistdocs.com -- Downloaded: 2009-07-16T13:55Z Check the source to verify that this is the current version before use.
Page 1 and 2: [lNCti-POUNDl MIL-HDBK-244A 6 APRIL
Page 3 and 4: MIL-HDBK-244A CONTENTS PARAGRAPH 1.
Page 5 and 6: MIL-HDBK-244A CONTENTS PARAGRAPH ~
Page 7: MIL-HDBK-244A CONTENTS PARAGRAPH 5.
Page 11 and 12: MIL-HDBK-244A CONTENTS PARAGRAPH pA
Page 13 and 14: MIL-HDBK-244A CONTENTS FIGURE L 3.
Page 15 and 16: 2.1 Government documents. MIL-HDBK-
Page 17 and 18: MIL-HDBK-244A STANDARDS MILITARY MI
Page 19 and 20: MIL-HDBK-244A 2.1.2 Other Governmen
Page 21 and 22: MIL-HDBK-244A PUBLICATIONS -.Contin
Page 23 and 24: MIL-HDBK-244A 3. DEFINITIONS 3.1 Ai
Page 25 and 26: MIL-HDBK-244A 3.12 . Se~aration. Th
Page 27 and 28: MIL-HDBK-244A 4. GENERAL REQUIREMEN
Page 29 and 30: MIL-HDBK-244A 5. DETAILED REQUIREME
Page 31 and 32: MIL-tlDBK-244A aircraft. The aerody
Page 33 and 34: MIL-HDBK-244A available. Unfortunat
Page 35 and 36: MIL-HDBK-244A -1 (g) Employment,par
Page 37 and 38: MIL-HDBK-244A (m) Shock effects -,O
Page 39 and 40: MIL-HDBK-244A plane which isparalle
Page 41 and 42: ,MIL-HDBK-244A difficulty as MIL-ST
Page 43 and 44: MIL-HDBK-244A (e) DC signal - volts
Page 45 and 46: MIL-HDBK-244A (f) Alignment - The a
Page 47 and 48: MIL-HDBK-244A to the suspension equ
Page 49 and 50: MIL-HDBK-244A 5.1.6.2.1 Mechanical
Page 51 and 52: MIL-HDBK-244A 5.1.7.2.2 Internal ca
Page 53 and 54: MIL-HDBK-244A (e) Side-by-sideor ta
Page 55 and 56: MIL-HDBK-244A 5.1.8.3 Thermal. Desi
Page 57 and 58: MIL-HDBK-244A In addition, DOD-HDBK
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MIL-HDBK-244A 5.1.9.2.4 : Foreicm o
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65 60 r 60 * 2’ 0 c .- 55 50 45 .
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MIL-”HDBK-244A 5.1.10.3.1 Aircraf
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The’140 dB the muzzle muzzle and
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MIL-HDBK-244A 5.1.10.6.6 Pitch or v
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MIL-HDBK-244A prior to any internal
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MIL-HDBK-244A (d) Double-feed - Thi
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MIL-HDBK-244A 5.2.1 Sha~e criteria.
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MIL-HDBK-244A with high ‘fatigues
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MIL-HDBK-244A 5.2.8 Store/loadingan
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5.2.10 Conflagration hazards. MIL-H
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MIL-HDBK-244A (b) Will not be suppo
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MIL-HDBK-244A . (c) Dispensers (1)
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MIL-HDBK-244A 5.3.7.2 ~. The drag o
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. MIL-HDBK-244A (1) Finned - As a g
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MIL-HDBK-244A shield braid.for EMI
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MIL-HDBK-244A could”be categorize
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.MIL-HDBK-244A MIL-A-8591,’MIL-M-
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MIL-HDBK-244A Air Force - AFSCDH 1-
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MIL-HD13K-244A 5.3.13.1.7 Externalp
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MIL-HDBK-244A 5.3.15 Reliability an
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MIL-HDBK-244A (b) SMS to power syst
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MIL-HDBK-244A in determining the in
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MIL-HDBK-244A of the aircraft. (d)
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MIL-HDBK-244A TABLE 11. Wind tunnel
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MIL-HDBK-244A 6.1.3.2 Ejector perfo
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MIL-HDBK-244A TABLE III. Vibration
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MIL-HDBK-244A 6.1.5.1 Enuineerina a
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MIL-HDBK-244A allowed by the procur
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MIL-HD8K-244A in any group, all sto
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MIL-HDBK-244A 6.1.7 Aeros~ace cwoun
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MIL-HDBK-244A (h) Tool requirements
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MIL-HDBK-244A suitably instrumented
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MIL-HDBK-244A (a) The traditionalme
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MI,L-HDBK-244A 6.2.1.7.6 Part I/fir
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HIL-HDBK-244A al * -.. +’, 1 1 I
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MIL-HDBK-244A 6.2.2 Storese~aration
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MIL-HDBK-244A that same flight cond
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MIL-HDBK-244A store with all deck h
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,, MIL-HDBK-244A 7. REPORTINGAND DO
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MIL-HDBK-244A (3) Rate of-climb. (4
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MIL-HDBK-244A 7.2 ““ “ Intern
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. STANDARDIZATION DOCUMENT IMPROVEM
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