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