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MIL-HDBK-336 -1

SURVIVABILITY AIRCRAFT NONNUCLEAR, GENERAL CRITERIA-VOLUME 1

Organization:
AIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City
Year: 1982

Abstract: This is the first volume in a four-volume design handbook for nonnuclear survivability of military aircraft. Each volume is structured to be used in conjunction with the other three volumes, as needed, in the design process. This volume contains general information pertaining to vulnerability and survivability analysis techniques, weapon terminal effects, computer program descriptions, and basic subsystem conceptual design concepts. Volume 1 is arranged in a manner that allows the user to easily identify the specific information of interest.
The data contained in this design handbook have been arranged to support the development of both fixed and rotary wing military aircraft. Each has unique mission and performance characteristics that require specialized attention and design solutions. The subsystem design categories have been established with these considerations in mind. For example, the power train and rotor blade subsystems deal primarily with military helicopter applications, while the launch/recovery systems deal with those subsystem elements for both fixed and rotary wing aircraft landing gear systems and for those systems related to the assisted takeoff (launching) and deceleration (recovery) methods most used by the Air Force and Navy fixed-wing aircraft.
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URI: http://yse.yabesh.ir/std;query=autho1279ear793325273135A68A10958014A/handle/yse/65657
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contributor authorAIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City
date accessioned2017-09-04T16:02:28Z
date available2017-09-04T16:02:28Z
date copyright30249
date issued1982
identifier otherRNSSDAAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=autho1279ear793325273135A68A10958014A/handle/yse/65657
description abstractThis is the first volume in a four-volume design handbook for nonnuclear survivability of military aircraft. Each volume is structured to be used in conjunction with the other three volumes, as needed, in the design process. This volume contains general information pertaining to vulnerability and survivability analysis techniques, weapon terminal effects, computer program descriptions, and basic subsystem conceptual design concepts. Volume 1 is arranged in a manner that allows the user to easily identify the specific information of interest.
The data contained in this design handbook have been arranged to support the development of both fixed and rotary wing military aircraft. Each has unique mission and performance characteristics that require specialized attention and design solutions. The subsystem design categories have been established with these considerations in mind. For example, the power train and rotor blade subsystems deal primarily with military helicopter applications, while the launch/recovery systems deal with those subsystem elements for both fixed and rotary wing aircraft landing gear systems and for those systems related to the assisted takeoff (launching) and deceleration (recovery) methods most used by the Air Force and Navy fixed-wing aircraft.
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languageEnglish
titleMIL-HDBK-336 -1num
titleSURVIVABILITY AIRCRAFT NONNUCLEAR, GENERAL CRITERIA-VOLUME 1en
typestandard
page223
statusActive
treeAIR FORCE - 71 - Air Force Sustainment Center - Oklahoma City:;1982
contenttypefulltext
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