MIL-S-23069A(As)
3.5.1 Current rating. EEDs having a no-fire current rating less than 1
ampere shall not be used.
3.5.2 Circuit isolation requirement. The firing circuits in an EED shall be
isolated front any metallic case or enclosure of the EED.
3.5.3 Barrier requirements. A continuous insulating barrier shall be
provided between all parts of the firing circuits in an EED and its case.
This barrier shall be of suitable plastic or other stable, inert
noncontaining
material having high resistivity and dielectric strength.
3.6 Warhead hazard-tests. At all times the handling of high explosives shall
be governed by the basic guidelines of DOD 4145.26M. All warheads shall be
subjected (at a minimum) to the safety test series of DOD-STD-2105(NAVY),
"Hazards Assessment Test for Navy Nonnuclear Ordnance," and shall meet its
passing criteria. When warheads are loaded with explosives not previously
approved for service use, the new explosive shall be subjected (at a minimum)
to the satety test series of DOD-STD-2105(NAVY) and NAVORD 0D 44811 Volume 1,
"Safety and Performance Tests for Qualification of Explosives." When
qualification of a new explosive is intended (versus qualification of the
warhead) the new explosive may be tested in. a container simulating the
warhead. When qualification of a warhead is intended, the warhead itself must
be used. A container loaded with explosives simulating the warhead shall not
be used.
3.6.1 Free fall tests. Free
fall tests from a height of 40 feet on a flat
plate or from 10 feet onto a
similar plate fitted with one inch studs shall be
conducted in accordance with
MIL-STD-331. The warhead shall be safe to handle
and dispose of following
the drop tests. . .
3.6.2 Ballistic penetration or impact requirement. The warhead shall not
detonate when penetrated by a 20mm AP projectile at service velocity, or by an
impact from fragments from 20mm Ap rounds or from missiles, either
surface-to-air or air-to-air.
3.6.3 Temperature requirement.
The warhead shall be so designed as to
preclude hazards resulting from
aerodynamic heating within the extremes of the
temperature environment of the
missile system. A specific test shall be
conducted to simulate the worse
case profile of the temperature expected.
3.6.4 Service life environment requirement In the design of the warhead,
consideration shall be given to variations encountered, such as: submerged
stowage heat from aircraft engines, sustained operation at low temperatures
and effects of aging The warhead explosive material shall be insensitive to
heat and incorporate insulation to delay explosive reactions which exposed to
aircraft fuel fires (see MIL-STD-1648).
3.6.5 Vibration environment requirement. The equipment shall be designed to
withstand any vibrations experienced in normal transportation by rail, truck,
sea or air shipment as well as vibration aboard the launch aircraft. The
tests shall be conducted in accordance with DOD-STD-2105(NAVY).
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