MIL-M-8555C
Performance
b.
(1)
Bandwidth
Error slope (the error slope is defined as the ratio of the
(2)
incremental change in apparent target position to an equal change
in look angle).
Transmission and reception signal losses.
(3)
Erosion and absorption.
(4)
Thermal tolerance.
(5)
Strength.
(6)
3.9.1.2 Antenna(s). The following parameters and characteristics of
each antenna contained in the missile shall be specified (see 3.9.5.4 for fuze
receiving and transmitting antennas):
Physical characteristics
a.
(1)
Type of antenna (planar, parabolic, etc).
(2)
Polarization.
Mixer design, if it is a part of the antenna.
(3)
(4)
Gimbal design and limits,
(5)
Antenna stabilization designs
(6)
Dimensions.
(7)
Height.
b. Performance
(1)
Sum and difference pattern versus frequency
(2)
Coupling losses.
Peak power limit, if it is a transmitting antennas
(3)
(4}
Frequency bandwidth.
(5)
Antenna stabilization response and accuracy,
3.9.1.3 Transmitters}. The following parameters and characteristics of
each transmitter contained in the missile shall be specified:
Physical characteristics
a.
(1)
Type of transmitter (impatt diode, magnetron, etc.
(2)
Modulator design,
(3)
Dimensions,
(4)
Weight,
(5)
Power required.
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