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| MIL-T-18232B(AS)
3.14.6
STABILIZATION SYSTEM. - The stabilization system shall be
suitable for all specified target airspeeds, altitudes,
maneuvers, flight and environmental conditions required by the detail specification.
3.14.7
RADAR AUGMENTATION. - Radar augmentation devices or equipment
shall be provided as specified in the detail specification.
Suitable scale model tests shall be made to verify the radar cross-section that
the target represents. Additional test shall be required where augmentation
devices (either active or passive) are required.
3.14.8
INFRA-RED AUGMENTATION. - Infra-red augmentation shall be
provided as specified in the detail specification.
3.14.9
MISS-DISTANCE INDICATING EQUIPMENT. - Miss-distance indicating
equipment shall be provided as specified in the detail specific-
ation.
3.14.10
TELEMETERING. - When telemetering is required, the smallest
and simplest system practicable shall be used which will
reliably provide the required data. Telemetering equipment shall conform to
Inter-Range Instrumentation Group (IRIG) standards. The telemetering system shall
operate with the recording station designated by the procuring activity. The
telemetering transmitter shall radiate the minimum power commensurate with reliable
operation under all operating conditions. The telemetering system shall be so
designed that there will be no deleterious interference between it and other sys-
tems within the target. The telemetering equipment shall be capable of withstand-
ing all the environments which the target may encounter. The equipment shall be
designed to be as rugged as arid to have equal or greater precision than, the
equipment it is expected to test. The selection of telemetering equipment shall
be in accordance with the "Navy Department Guided Missile Telemetering Standardiza-
tion Program" and subject to approval by NAVAIR.
3.14.11
RADOMES. - Radomes shall be in accordance with specification
MIL-R-7705.
3.14.12
ANTENNAS. - Antenna and antenna systems shall present minimum
aerodynamic drag consistent with the equipment and target
performance requirements. Antenna lead-ins shall be of minimum or specified
lengths and so routed as to minimize coupling of interference from nearby sources.
Design aims shall be as follows:
(1) Antenna mechanical design and location shall represent an
optimum compromise between weight and drag taking into account
the required range, speed} size and aerodynamic performance of the target. If the
weight of a zero drag antenna is more of a penalty on fuel or range or both, than
a lighter weight, plus the drag, of an external antenna is on fuel, range, or
aerodynamic performance, then the best compromise shall be effected consistent
with the electrical requirements.
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