MIL-HDBK-244A 6 apr 90.pdf

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MIL-HDBK-244A CONTENTS PARAGRAPH 4. 4.1 4.2 4.2.1 4.2.2 4.2.3 4.2.4 4.3 GENERAL REQUIREMENTS................................... Basic design areas..● ......● ....................● ..... Types of compatibilityrequirements.................. Type I................................................ Type II...............● ........................,..... TyPe III.............................................. Type IV............................................... Compatibility at the design stages.........i......... PAGE 14 14 14 14 _ 15 15 ,:: ; ;:1 5.1.1 5.1.1.1 5.1.1.1.1 5.1.1.1.2 5.1.1.1.2.1 5.1.1.1.2.2 5.1.1.1.2.3 5.1.1.1.2.4 5.1.1.1.2.5 5.1.1.1.2.6 5.1.1.1.2.7 5.1.1.1.2.8 5.1.1.2 5.1.1.2.1 5.1.1.2.2 5.1.1.2.3 5.1.1.2.3.1 5.1”.1.2.3.2 5.1.1.2.3.2.1 5.1.1.2.3.2.2 5.1.1.2.3.2.3 5.1.1.2.3.2.4 5.1.1.2.3.2.4.1 ..5.1.1.2.3.3 5.1.2 5.1.3 5.1.3.1 DETAILEDREQUIREMENTS..:..... .......................... Aircraft design...................................... Store installationcriteria......*................... .Carriage...*:.● : ● ..................................... Mission requirements.........● ...*.............-- ...’”. ----- Selecting carriage location of airframe..........~... Performance....................● ..................... Stability and control................................ Lifting and control surfaces......................... Engine inlets....................**.................. Airframe functional components and’systems........... Boundary layer disturbancesor separation............ Stability.and control during store’separation........ Preflight access panels .............................. , Separation,*......................*................... Separation during design phase....................... Separation problem area.............................. Separation analysis.................................. Factors.............................................. Separation analysis data............................. Analytically derived data’............................ Suspension equipment data............................ Experimental data...*......● ...................● ● .... Six degrees of freedom computer analysis............. Choice of axes system.........................’...... Separation criteria.................................. Store-to-aircraftclearances and fit................. Electrical interface................................. Categories........................................... 16 - 16 16 “16 16 17 17 17 17 18 18 18 18 18 19 19 ;: 20 24 24 24 24 25 25 25 27 27 27 iv . . 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 ~ 5.1.3.2 5.1.3.3 5.1.3.4 5.1.3.5 5.1.3.6 5.1.3.7 5.1.4 5.1.4.1 5.1.5 5.1.5.1 5.1.5.1.1 5.1.5.1.1.1 5.1.5.1.1.2 5.1.5.1.2 5.1.5.2 5.1.5.2.1 5.1.5.2.2 5.1.6 5.1.6.1 5.1.6.2 5.1.6.2.1 5.1.6.3 5.1.7 5.1.7.1 5.1.7.1.1 5.1.7.1.2 5.1.7.1.2.1 .5.1.7.1.2.2 5.1.7.1.2.3 5.1.7.2 5.1.7.2.1 5.1.7.2.2 5.1.7.2.2:1 5.1.7.2.3 5.1.7.2.3.1 5.1.7.2.3.2 5.1.7.2.4 5.1.8 5.1.8.1 5.1.8.2 5.1.8.3 5.1.8.4 5.1.8.5 5.1.8.5.1 5.1.8.5.2 5.1.8.5.3 5.1.8.5.4 Logistics and training............................... 28 Multiplex circuits................................... 28 Test circuits........................................ 29 Electrical connectors..............................“. 29 ._ Pin function assignment.............................. Location of electrical disconnects................... :: Electrical release systems design.................... 30 Guidelines for armament systemsafety................ 30 Mechanical interface................................. Safety devices....................................... ;; In-flight............................................ 33 Interlocks........................................... 33 Jettison............................................. 33 Ground..................................● ......’:.”... .-.. 33 Accessibility........................................ 34 Loading or off-loading...............................’ 34 Checkout’and preparation............................. 35 Aircraft structure................................... Carriage loads....................................... ;: Flutter and vibration................................ 35 Mechanical instability............................... 36 Landing loads......● ...● ...............● ...● ........ 36 ● Aerodynamics......................................... 36 Flying qualities..................................... 36 Store carriage locations............................. 36 Store carriage and separation aerodynamics........... Stability with external carriage..................... :; Stability with internal carriage..................... ~ 37 Engine ingestion of missile exhaust.................. 37 Optimizing carriage aerodynamics............... ..... 37 Choosing carriage class.............................. 37 Internal carriage aerodynamics....................... 38 Weapon bay design.................................... 38 External carriage aerodynamics....................... - 39 Wing mounted stores.................................. 40 Pylon design parameters”.............................. 40 Drag count (index) system............................ 41 Environment.......................................... 41 Store related equipment within aircraft.............. 41 Aeroacoustic or acoustic............................. Thermal.............● .......● ........................ % Nuclear hardening.................................... 42 Electromagnetic...................................... 42 Design guidance...................................... 43 Electroexplosivesubsystems.......................... 43 Electromagneticinterference......................... 43 Electrical bonding and lightning protection.......... 46 Source: http://www.assistdocs.com -- Downloaded: 2009-07-16T13:55Z Check the source to verify that this is the current version before use. v
Page 1 and 2: [lNCti-POUNDl MIL-HDBK-244A 6 APRIL
Page 3: MIL-HDBK-244A CONTENTS PARAGRAPH 1.
Page 7 and 8: MIL-HDBK-244A CONTENTS PARAGRAPH 5.
Page 9 and 10: 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
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MIL-HDBK-244A 5.1.8.3 Thermal. Desi
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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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