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MIL-T-18232B(AS)
3.6.1.1
DESCRIPTION. - The fuselage shall include all equipment
compartments.
CONSTRUCTION. - Construction of the fuselage shall meet the
3.6.1.2
requirements specified herein and in the detail specification.
3.6.1.3
EQUIPMENT COMPARTMENTS. - Equipment compartments (electronic
equipment compartments, etc.) shall be provided as required
by the detail specification.
LAUNCHING AND RECOVERY
3.7
3.7.1
LAUNCHING PROVISIONS
3.7.1.1
AIR LAUNCHING. - Suitable provisions shall be made for attach-
ment to, carrying on, and release/ejection from the store
suspension equipment normally fitted on the launching aircraft. A list of air-
craft with which compatibility is required will be included in the system detail
specification. Specification MIL-A-8591 shall be complied with where applicable,
consistent with the launching arid handling provision of the system detail specifi-
cation. The design shall be capable of meeting the requirements of specification
MIL-T-7743.
3.7.1.2
CATAPULTING. - Provision for catapulting shall be in accord-
ance with the detail specification.
3.7.1.3
JET-ASSISTED TAKE-OFF. - Provision shall be made, as required
by the detail specification and in accordance with Specifica-
tion MIL-J-8667, for the attachment of jet-assisted-take-off (JATO) units. This
provision shall include all reinforcements and fittings necessary to attach the
units, electrical wiring, switches and auxiliaries for firing, and provision for
releasing and jettisoning the units. The JATO attachment system shall not require
alignment on the target.
3.7.2
RECOVERY
3.7.2.1
RECOVERY SYSTEM. - The air recovery system includes parachute,
riser cables, attaching Fittings, release and door actuating
mechanism.
3.7.2.1.1
PARACHUTE. - A parachute of approved type and suspension gear
shall be provided to permit normal air recovery in accordance
with MIL-P-25062 with a minimum damage to the target. The parachute shall be
suitable for lowering the target at a maximum sinking speed of 18 feet per second
at sea level with 25% of maximum fuel aboard. Adequate flotation shall be incor-
porated in the parachute assembly to insure that the parachute will remain afloat
for one hour after release from the target.
28

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