Flexible Confined Detonating Cord Assembly - Ensign
Transcription
Flexible Confined Detonating Cord Assembly - Ensign
Flexible Confined Detonating Cord Assembly (FCDCA) PRODUCT TECHNICAL DATA SHEET DESCRIPTION: Flexible Confined Detonating Cord Assembly (FCDCA) is a linear explosive component widely used in the aerospace industry for detonating signal transfer. The device consists of a linear explosive cord, wrapped in a flexible confinement tube which has end tips that can be connected into manifolds or other ordnance devices. KEY FEATURES: • Provides confinement of the ordnance event and gaseous products • Insensitive to unintended ignition from mishandling or ballistic damage • Rugged, flexible and lightweight APPLICATION: PROPERTIES: • Fully proven on Tactical Missiles, • Hermetically sealed and tested to a wide Strategic Missiles and Space Launch Vehicles range of temperatures • Ideal for systems that require a robust, • Available in any length and with numerous high-strength, flexible energy transfer line end tip types and thread sizes • Designed to withstand demanding aerospace • Lockwire provisions come standard environmental conditions • RCC 319 Range Compliant • Ideal for installations with tight bend radii ENSIGN-BICKFORD AEROSPACE & DEFENSE COMPANY www.EBA-D.com Cleared for Open Publication by the Office of Security Review, Department of Defense 4/25/2013 13-S-1629 Fuzes Detonating, UN0367 1.4S Flexible Confined Detonating Cord Assembly (FCDCA) SPECIFICATIONS: Qualification Test Levels Thermal Cycle 24 Cycles, 2 Hour Dwells at -65˚F to 160˚F (-54˚C to 71˚C) Thermal Vacuum 15 Cycles at -66˚F to 212˚F (-54˚C to 100˚C), 12 Hour Dwells at 1 x 105 Torr (0.0013 Pa) High/Low Temperature Function 250˚F (121˚C) High and -309˚F (-198˚C) Low Pyrotechnic Shock 31,000 G Peak, 3 Axis, 3 Shocks/Axis Random Vibration 220.5 Grms, Lateral Axis, 270 Sec/Axis 206.0 Grms, Radial Axis, 30 Sec/Axis Axial Loading (Pull Test) 100 Lbf (445 N) for 60 Sec Drop Test 6 Foot (1.83m) Drop, 40 Foot (12.19m) Drop High Temperature Storage 60 Days at 160˚F (71˚C), 40-60% RH Per MIL-STD-1576, Method 3403 for 10 year service life Humidity 4 Cycles of 95˚F (35˚C) at 95% RH and 35.6˚F (2˚C), 2 Hour Dwells Per MIL-STD-810 Method 507.3 Construction: Explosive End Tips: •Type I and Type III end tips containing HNS-1A. MDF Cord Materials: • The explosive cord consists of an aluminum sheath containing HNS-IIA explosive. Overwrap and Braiding Materials: • Tefzel® Thermoplastic Elastomer, Kevlar® and Stainless Steel. Free Spinning Threaded Nuts: • Enable the FCDCA to be fastened into a manifold or other device. • Different diameters and thread sizes to prevent incorrect installation. OPERATION: A detonation is required to initiate the FCDCA, which enables a detonating signal to be transmitted along the length of the Mild Detonating Fuse (MDF) cord where it is output from the tip at the opposite end. Manifolds may be used as interfaces to distribute the signal from one FCDCA to another. The FCDCA transmits a detonating signal from an ordnance initiating device to an output device such as a Destruct Charge, Linear Shaped Charge or Frangible Joint. ENSIGN-BICKFORD AEROSPACE & DEFENSE COMPANY 640 HOPMEADOW STREET, P.O. BOX 429, SIMSBURY, CT 06070, USA www.EBA-D.com ENSIGN-BICKFORD AEROSPACE & DEFENSE COMPANY Kevlar and Tefzel are registered trademarks of DuPont. 640 HOPMEADOW STREET, P.O. BOX 429, SIMSBURY, CT 06070, USA www.EBA-D.com ® ® Attention: The information and recommendations described in this brochure cannot possibly cover every application of the products or variation of conditions under which the products are used. Attention: The information andonrecommendations described in this brochure possibly cover everytoapplication of the or variation of conditions which the products are used. The The recommendations herein are based the manufacturer’s experience, research andcannot testing. They are believed be accurate, butproducts no warranties are made, express orunder implied. In addition, the specifications recommendations herein arerepresent based on our the current manufacturer’s experience, research and testing. They are believed to be accurate, but to nocontact warranties are made, express or implied. In addition, theforspecifications contained herein are all nominal which production. The products described may be subject to change. Please feel free Ensign-Bickford Aerospace & Defense Company verification. contained hereinThe areproducts all nominaldescribed which represent ourare current production. The products described may be subject to change. Please feelbyfree Ensign-Bickford Aerospace & Defense Company for verification. No Warranties or Liabilities: herein sold “AS IS” and without any warranty or guaranty, express, or implied, arising lawtoorcontact otherwise including without limitation any warranty of merchantability No Warranties or Liabilities: The products herein are sold IS” and without anyany warranty guaranty,whatsoever express, orarising implied, law or otherwise including without limitation warranty of merchantability or fitness for a particular purpose. Buyer and userdescribed agree further to release and“AS discharge seller from and allorliabilities outarising of theby purchase or use of any product described hereinany whether or not such liability is or fitness for occasioned a particular by purpose. and user agreesupon further to release discharge seller from anyofand all liabilities whatsoeverContent©2013 arising out of the purchase or useAerospace of any product described herein whether or not liability is seller’sBuyer negligence or based strict productsand liability or upon principles indemnity or contribution. Ensign-Bickford & Defense Company, Simsbury, CTsuch 06070, U.S.A. occasioned by seller’s negligence or based upon strict products liability or upon principles of indemnity or contribution. Content©2011 Ensign-Bickford Aerospace & Defense Company, Simsbury, CT 06070, U.S.A Cleared for Open Publication by the Office of Security Review, Department of Defense 4/25/2013 13-S-1629