AIR FORCE MIL-HDBK-336-1-1982 SURVIVABILITY AIRCRAFT NONNUCLEAR GENERAL CRITERIA-VOLUME 1《一般标准-第1卷飞机非核生存力》.pdf

1、MILITARY MIL-HDBK-336-1 25 October 1982 HANDBOOK SURVIVABILITY, AIRCRAFT, NONNUCLEAR, GENERAL CRITERIA-VOLUME 1 NO DELIVERABLE DATA REQUIRED BY THIS DOCUMENT Fse Mise Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-UTT unnv _ “l “lL_ 1 Ll.L.lI-nV.LJC

2、.- JJV-.L MIL-HDBK-336-1 DEPARTMENT OF DEFENSE WASHINGTON 25, DC Military Handbook for Aircraft Nonnuclear Survivability. 1. This standardization handbook was developed by the Department of Defense with the assistance of the Air Force Wright Aeronautical Laboratories (AFALiFIE) in accordance with es

3、tablished procedure. 2. This publication was approved on 26 October 1982 for printing and inclusion in the military standardization handbook series. 3. This document provides basic and fundamental information on military aircraft survivability design requirements and assessment methodology. It will

4、provide valuable information and guidance to personnel concerned with and assessment of military aircraft. The handbook is not intended to -.:-L1U: ut:o .L.01l be re-ferenced in purchase specifications except for informal purposes nor shall it supersede any specification requirements. 4. Every effor

5、t has been made to reflect the latest information on military aircraft design techniques and assessment methodology. T . .t_ 1-_ .L.L .L.O LUt: intent to review this handbook periodically to insure its completeness and currency. Beneficial comments (recommendations, additions, deletions) and an pert

6、inent data which may be of use in improving this document should be- addressed to: (Air Force Systems Command, Attn: ASD/ENESS, Wright Patterson Air Force Base, Ohio 45433) by using the self-addressed Standardiza tion Document Improvement Proposal (DD Form 1426) appearing at the end of this .l _ _ .

7、 _ . . 1 _ _ UULUlllt:UL UJ. uy .L.t:LI.-t:1 ii Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-HDBK-336-1 FOREWORD 1. This is a four volume ilitary Handbook. The titles of the four volumes are: a. Volume - Survivability; Aircraft Nonnuclear, Gen

8、eral Criteria b. Volume 2 - Survivability, Aircraft, Nonnuclear, Airframe c. Volume 3 - Survivability, Aircraft, Nonnuclear, Engine d. Volume 4 General Criteria The information contained in volumes 1, 2, and 3 is unclassified to permit greater utilization and accessibility to the user. In areas wher

9、e classified data is applicable, it has been incorporated into volume 4, and is referenced as such in the text of each volume. 2. This handbook has been prepared to provide military planners and industry with the information and guidance needed for the conceptual and detail design of the new aircraf

10、t where nonnuclear-survivability enhancement is to be inte grated into the system. It is also structured to provide data and guidance for the incorporation of survivahility-enhancement features into existing aircraft systems as a retrofit modification. Both fixed and rotary wing aircraft design info

11、rmation are contained in this publication. Figure 1 illustrates the role of this handbook in the design process. It is a task-flow diagram of the major elements involved in the development of new aircraft. The system requirements are initiated by the using command that defines the operational requir

12、ements and capabilities desired to perform specific combat missions. These requirements are studipd hv r-hp nnrnnr;:Irp c:pr,;rp :IC1pnr;pc: ;n rnp f“,rm “,f r“,nrpnt-1!:Il -J - -rr-r- - . -_- -0- - - _ -. - -.a-r-(Phase 0) design analyses. The optimum mission and performance parameters are defined

13、t along with system/cost effectiveness comparisons of candidate concep tual design candidates. This is accomplished through an analysis to identify the mission-essential functions that must be performed in order to accomplish the specific mission objectives. With these functions defined, an analysis

14、 is conducted to identify the subsystem-essential functions that must be provided to perform the mission-essential functions. At the same time an analysis is conducted to identify the hostile threat systems to which the aircraft system may be expected during the conduct of its operational mission. T

15、he results of these analyses are then used by the S/V engineer to conduct an evaluation of the various candidate survivability-enhancement techniques that may be used in the design concepts. This design handbook will be the basic source for identi fication of the basic principles and techniques that

16、 may be employed. It will also provide references to other information sources for more detailed and/or specialized data. The results of this analysis are summarized into recommenda tions for the development of candidate conceptual aircraft designs. As each _ .lJ_ _ LdlluuaLe system is evolved, vuln

17、erability and survivability assessment are conducted t-“, l:.,rl1t!t-Q t-ho oFFo,t-4“.o. o“ ,F t-ho-4, ,1.; y,1,. l t:./U ,1Oc!“ Fot-1toC! - _, -A“ . - “,l;t-u ccoccmaTlr (t“mTl1rPT ml“lt1plc;: _ YU1.j,.U:) L;:) 1 r“l“l 1 L Tnnllt- rl“,t-:. t 4 ?c:;.c:;. I 256 257 I 258 I 259 260 )t:l r “-V.L 262 II

18、 263 264 I 265 I 266 I 2-4 j f Volume Number ( I I I J I I I I I I X i I I I X I I I I X II I I I X I I I X I I I I I I I X I I , X ,I I I X I I I I I ,I I I X I I X I I I I I I I I I X I I I X I I I X I , I I I, I I X I I I X I I I I X II I I I X I I I X I I I I X I I I I I I I Provided by IHSNot f

19、or ResaleNo reproduction or networking permitted without license from IHS-,-,-M1L-HDBK-336-1 2.3 Reference by subject. Table 2-11 lists the References by subject matter. TABLE 2-11. References by subject matter Category I I il) . 00 u Ul . . I-l 0 - (1) I-l (1) 0 I-l “ rn -1 tl (1) :J s (1)-1 :l e e

20、 I-l (1) (1) :J 0 o -4 rl X I-l rl “ I-l o.c No. -(J) o x x x “-.J -J “-.J “-.J .pLJNI- : .-1 X x X xxxx xx:xx .- 00 00 00 eX) 00 00 1 -.J -.J -.J VI.s:-WN_ OC)(X)-.JO X -: : X xxx xx X M ) I H H General Structures Personnel (Crew) . I ro Fuel Propulsion Power Train I I Rotor Blades Flight Cont. Flu

21、id Power = n ro H w I : w C I a u. w m n I rt L Envir. Cont. rt rt Oxygen 11 Armament n 0 Elect. Power “ Avionics Launch/Recov. c , Armor Computer Prog. Threat Datal Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-1.: II 10 1- N NN Nt-.;) VI.P-WNI- X

22、 X X XX X X -. 1- . NI- . 01000 XXX X XXX -. . X . . . . . . Q VI l.oJ N . X X : I n o :1 rt . ,. :1 c: ttl elL. 3: H t“ I ;:x: t:I OJ ?: I w W Q I Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-HDBK-336-1 TABLE 2-11. References by subject matte

23、r (continued) Category I I . OD u (I) . . J-I 0 - c (l) .,; J-I .,; (l) 0 J-I rd en C:.-1 -0 c: QJ c: :J u p,.,; Q)r-4 0 rd rd 0 0 0 Q) rd J-I Q) .-1 J-I r-4U 0 U .u p, (1)0: J-IO :l C enH cx:I p, C U -Q) rd .,; C r-4 .,; . c (l) .-1 c: .,;.,; Ref. s. u 0 = ,.,. ,.,. : “0 $./ QJ e .,; c: u ,.,. = rd

24、 Q) :l en r-4 p.Q) 0 OD OM oM ODrd u 0 C 0 p.Q) No. e j.; j.; QJ 0 .u :l : e aJ . :l S S 0 Q) .j) Q) = J-I 0 o r-4 r-4 C r-4 rd J-I oc: C)U)p, p,p, O: WO QJ 0 C :l U 0 0 Q) U 4-J P-. (I 0: C U - C QJ -1 .c Q) a 4-J C U I“f 00 tU U 0 C : S QJ -1 :s C :XX X -C“,- -4-: : :CXOO WNt-I : “ , “ “ 00 (XI “0

25、“1 : Z:;d / o (1) H General Structures Personnel (Crew) Fuel Propulsion Power Train Rotor Blades Flight Cont. Fluid Power Env:lr. Cont. Oxygen Arm.ament Ele1ct. Power Avionics Launch/Recov. Armor Computer Pro. Threat Data o 01 rt fD OQ o 11 : H G; t“4 trI N I H H (1) H (1) 11 (1) :t () 3: (1) 1-1 Cfl t-I I c:r = t:= Cfl c: , c:r w II IAJ a-t rt rt rt (1) 11 -, () 0 :t rt J-Io :t c: (1) 0 -“ Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-