ACT4407N datasheet(5/9 Pages) AEROFLEX

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SCD4404N Rev D 12/19/07

Aeroflex Plainview

Notes:

1. VCC = +15VDC ±0.75V, VEE = -15VDC ±0.75V, VIL = +5VDC ±0.5V, TC = -55°C to +125°C, unless otherwise specified.

2. All typical values are measured at +25°C.

3. Characteristics guaranteed by design, not production tested.

4. Power ON/OFF, measured from 75KHz to 1MHz at Point A-A' Figure 4, in accordance with MIL-STD-1553B paragraph 4.5.2.2.2.3.

5. At point A-A' on Figure 3 or 4, 2.5µS after midpoint crossing of the parity bit of the last word of a 660 µS message.

6. Receiver skew is defined as the time from the rising edge of RX DATA OUT to the rising edge of RX DATA OUT minus 500 nS, with a

sine wave input of 3 VP-P at 1MHz driven into Point B-B' of Figure 4 or 2.1 VP-P at 1MHz driven into Point B-B' of Figure 3. The

specification maximum is guaranteed for TA = 25°C only. Standard TTL loads applied to RX DATA Outputs.

7. This test is performed while the Transceiver is reading its own transmission. This condition is called "Wraparound". Standard TTL loads

applied to RX DATA Outputs.

TYPICAL HYBRID POWER DISSIPATION

Power Supply Conditions

Condition

Standby

100% Duty

Cycle

Unit

PSC1

VCC = +15V

VEE = -15V

VL = +5V

Point B-B', ZO = 70 Ω, VO = 29 VP-P

Bit Pattern = FFFF

HEX

Figure 4

0.540

2.167

Watts

PSC2

VCC = +15V

VEE = -12V

VL = +5V

0.465

1.852

PSC3

VCC = +12V

VEE = -12V

VL = +5V

0.450

1.600

* See Aeroflex Application note# 112 for reference.

Recommended Power Supply Voltage Range

+11.4 Volts to +15.75 Volts

-V

-11.4 Volts to -15.75 Volts

Logic

+4.5 Volts to +5.5 Volts

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