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MIL-DTL-32183

CATAPULT, AIRCRAFT EJECTION SEAT: CKU-5C/A REWORK ASSEMBLY

Organization:
NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD)
Year: 2004

Abstract: This specification establishes the requirement for the refurbishment (rework) of the CKU-5C/A rocket catapults (ROCAT) for aircraft ejection seat assemblies. This specification includes only the requirements for restoration of salvageable hardware. All other requirements for the CKU-5C/A ROCAT are specified in the new unit specification, MIL-DTL-32127 and drawing 512-174-0068. The earlier versions of CKU-5C/A ROCAT, the CKU-5/A/A and CKU-5B/A, may be converted to the CKU-5C/A configuration during the rework. Intended Use: The CKU-5C/A Aircraft Ejection Seat Catapult Rework Assembly composed of new, reused, restored, and modified components as applicable and as described herein and when loaded with propellant, in accordance with MIL-DTL-32124 Type IV and drawing 512-174-0071 and a CCU-22B/A Impulse Cartridge, drawing 512-174-0069, will produce the catapult CKU-5C/A assembly. The catapult assembly is to meet the requirements of MIL-DTL-32127 and is intended to be used in conjunction with other propellant actuated devices in aircrew emergency escape systems used in jet aircraft. The CKU-5C/A is designed for use in military aircraft, and has no commercial application.
URI: http://yse.yabesh.ir/std;query=autho47037D83081DAC4261598F1EFDEC014A/handle/yse/205653
Subject: Explosives
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    MIL-DTL-32183

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contributor authorNAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD)
date accessioned2017-09-04T18:23:13Z
date available2017-09-04T18:23:13Z
date copyright38342
date issued2004
identifier otherIDODIBAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=autho47037D83081DAC4261598F1EFDEC014A/handle/yse/205653
description abstractThis specification establishes the requirement for the refurbishment (rework) of the CKU-5C/A rocket catapults (ROCAT) for aircraft ejection seat assemblies. This specification includes only the requirements for restoration of salvageable hardware. All other requirements for the CKU-5C/A ROCAT are specified in the new unit specification, MIL-DTL-32127 and drawing 512-174-0068. The earlier versions of CKU-5C/A ROCAT, the CKU-5/A/A and CKU-5B/A, may be converted to the CKU-5C/A configuration during the rework. Intended Use: The CKU-5C/A Aircraft Ejection Seat Catapult Rework Assembly composed of new, reused, restored, and modified components as applicable and as described herein and when loaded with propellant, in accordance with MIL-DTL-32124 Type IV and drawing 512-174-0071 and a CCU-22B/A Impulse Cartridge, drawing 512-174-0069, will produce the catapult CKU-5C/A assembly. The catapult assembly is to meet the requirements of MIL-DTL-32127 and is intended to be used in conjunction with other propellant actuated devices in aircrew emergency escape systems used in jet aircraft. The CKU-5C/A is designed for use in military aircraft, and has no commercial application.
languageEnglish
titleMIL-DTL-32183num
titleCATAPULT, AIRCRAFT EJECTION SEAT: CKU-5C/A REWORK ASSEMBLYen
typestandard
page14
statusActive
treeNAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD):;2004
contenttypefulltext
subject keywordsExplosives
subject keywordsLauncher
subject keywordsPropellant
subject keywordsRocket motor
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